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STEP 2, 23105

Orbit data source: Space-Track

STEP 2, 23105 is a payload satellite owned by USAF STP (US) in LEO that was launched on Thu, 19 May 1994 UTC via a PEGASUS/HAPS launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
23105, 1994-029A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
TRWC/CTA
Mission
Defense Technology
Bus & Motor
LEOSTAR T-200, Unknown motor
Mass
180 kg wet, 180 kg dry
Launch date (UTC)
1994-05-19 (32 years ago)
Launch vehicle
PEGASUS/HAPS
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 4 Pan, 1.5 m
Radar Cross Section
3.076 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 STEP 2
1 23105U 94029A   26228.38065446  .00001942  00000-0  18156-3 0  9991
2 23105  81.9375 112.4096 0083287  61.7072 299.2517 14.90971202728850
Epoch: 2026-08-16T09:08Z
TLE epoch observation values (Epoch: 2026-08-16T09:08:08.545Z)
Latitude
-0.00001°
Longitude
10.59599°
Altitude
569.923 km
Speed
7.591 km/s
True Right ascension
07h 29m 38s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:48:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
649.991 km
Perigee altitude
533.888 km
Semi-major axis
6,970.076 km
Eccentricity
0.00833
Inclination
81.9375°
RAAN
112.4096°
Arg. of periapsis
61.7072°
True anomaly
298.41478°
Mean anomaly
299.2517°
Eccentric anomaly
298.83366°
Mean motion
3.72981 °/min
Orbital period
96.52 mins
BSTAR
0.00018156
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