1 AMENDMENT NO. 10 TO ORBCOMM SYSTEM PROCUREMENT AGREEMENT This Amendment No.10 ("Amendment No. 10") to the ORBCOMM System Procurement Agreement is entered into this 30th day of September, 1999 between ORBCOMM Global, L.P. ("ORBCOMM Global") and Orbital Sciences Corporation ("Orbital"). WITNESSETH WHEREAS, the parties previously entered into the ORBCOMM System Procurement Agreement dated September 12, 1995 (the "Procurement Agreement") and Amendments No. 1, No. 2, No. 3, No. 4, No. 5, No. 6, No. 7, No.8 and No. 9 thereto; and WHEREAS, the parties wish to set forth their agreement on a change to the orbit parameters for the launch of ORBCOMM Plane D/ORBCOMM Launch 4 (previously known as the "Equatorial Plane") for which ORBCOMM Global has directed a change from the equatorial (zero degree) inclination launch to a 45 degree inclination launch using the Pegasus launch vehicle and a revision to the milestone payment schedule pertaining to such launch. NOW THEREFORE, the parties agree as follows: ARTICLE 1 - DEFINITIONS Terms used herein and not otherwise defined shall have the meanings assigned thereto in the Procurement Agreement. ARTICLE 2 - AMENDMENTS Section 2.1 Section 5.1(b)(v) of the Procurement Agreement shall be deleted in its entirety and replaced with the following: "(v) Satellites and Launch Vehicle No earlier than 5 Nov 1999 Launch Service No. 4" Section 2.2 Table 3.1 in Section 3.1.1 of Exhibit A, Part 1B Satellite Specifications of the Procurement Agreement shall be deleted in its entirety and replaced with the following: 2 " - ------------------------------------------------------------------------------------------------------------------------------------ Parameter Plane A Plane B Plane C Plane D - ------------------------------------------------------------------------------------------------------------------------------------ Target mean altitude 825 km, circular 818.5 km 818.5 km 825.0 km Maximum apogee altitude 882 km Target + 15 km Target + 15 km Target + 20 km Minimum perigee altitude 767 km Target - 15 km Target - 15 km Target - 20 km Target inclination 45 deg. 45.02 deg. 45.02 deg. 45.02 deg Inclination accuracy +/- 0.3 deg. +/- 0.1 deg. +/- 0.1 deg +/- 0.08 deg Target right ascension of 20 degrees East of ascending nodes Unconstrained 120 deg. East of Plane A 120 deg. West of Plane A Plane A Accuracy of ascending node N/A +/- 2.5 deg. +/- 2.5 deg. +/- 2.5 degrees Pegasus orbit performance capabilities assume a maximum satellite weight of 95 pounds each." Section 2.3 Table 3.1 in Section 3.1.1 of the Statement of Work and Specifications for the ORBCOMM-4 Launch Services (as originally set forth in Amendment No. 4 to the Procurement Agreement and as revised in Amendment No. 8 to the Procurement Agreement) shall be deleted in its entirety and replaced with the following: " ------------------------------------------------------------------------------ PLANE D/ORBCOMM-4 PARAMETER (45 DEGREE LAUNCH) ------------------------------------------------------------------------------ Target Mean Altitude 825.0 km ------------------------------------------------------------------------------ Maximum apogee altitude Target + 20 km ------------------------------------------------------------------------------ Minimum perigee altitude Target - 20 km ------------------------------------------------------------------------------ Target inclination 45.02 degrees ------------------------------------------------------------------------------ Inclination accuracy +/- 0.08 degrees ------------------------------------------------------------------------------ Target right ascension of 20 degrees East of Plane A ascending nodes ------------------------------------------------------------------------------ Accuracy of ascending node +/- 2.5 degrees ------------------------------------------------------------------------------ Semi-Major Axis +/- 12 km ------------------------------------------------------------------------------ ORBCOMM shall have at its disposal all available launch capacity of the Pegasus launch vehicle pertaining to the launch parameters set forth for the Plane D/ORBCOMM-4 mission." Section 2.5 Section 4.1(b)(iii) of the Procurement Agreement shall be deleted in its entirety and replaced with the following: 2 3 "(iii) Orbital shall be entitled to invoice ORBCOMM Global for costs associated with Section 3.1(d) as follows: PAYMENT DATE AMOUNT ------------ ------ October 1, 1998 $1,500,000 January 1, 1998 $2,000,000 April 1, 1999 $2,000,000 July 1, 1999 $2,000,000 October 1, 1999 $5,000,000 The Earlier of March 31, 2000 $8,000,000* or Launch of Fourth Plane September 30, 2000 $6,000,000 * If the launch is delayed beyond March 31, 2000 due to unavailability of the Satellites, Orbital shall be entitled to invoice ORBCOMM at the monthly rate of $1,000,000, beginning April 30, 2000, with the balance due on launch. In no event shall Orbital be entitled to invoice ORBCOMM in an amount to exceed $8,000,000." SECTION 3 - MISCELLANEOUS Section 3.1 This Amendment No. 10 shall be construed in accordance with and governed by the laws of the Commonwealth of Virginia, without giving effect to the provisions, policies or principles thereof related to choice or conflict of laws. Section 3.2 No changes to the Procurement Agreement are authorized hereby except as otherwise specified in this Amendment No. 10 IN WITNESS WHEREOF, the parties have executed this Amendment No. 10 as of the day and year first above written. ORBCOMM GLOBAL, L.P. By:___________________________________ Name: Scott L. Webster Title: Chairman and Chief Executive Officer ORBITAL SCIENCES CORPORATION By:___________________________________ Name: Richard J. Hampton Title: Senior Director, Contracts 3