Find STEP M2
NORAD ID: 23105 • Int'l Des: 1994-029 • Owner: STP • Country: US • operational
LEOCIRCULARPOLAR
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About STEP M2
STEP M2 (NORAD 23105) is a satellite launched May 19, 1994 by STP of US. It operates in LEO, CIRCULAR, POLAR orbit with a mass of 180.00 kg.
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Two-Line Element Set
1 23105U 94029A 26202.27325857 .00001792 00000-0 16797-3 0 9998
2 23105 81.9393 139.0654 0082783 146.1358 214.5186 14.90845765724964
Epoch: Jul 21, 2026 •
Age: 8 hours
Current Status
Altitude 666.8 km
Apogee / Perigee N/A
Velocity 7.49 km/s
Sub-Earth Point -36.28°S,
23.27°W
Launch Date May 19, 1994
Age 32.1 years
Type other
Technical Details
Classification Payload
Mass 180.00 kg
Dry Mass 180.00 kg
Total Mass 180.00 kg
Length 2.00 m
Diameter 1.00 m
Span 3.00 m
Shape Box + 2 Pan
Manufacturer TRWC/CTA
Bus Type LEOStar T-200
Phase Status In Orbit
Owner/State STP/US
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