Showing default

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.

Loading next visibility...
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: 7 hours ago

TLE from 7 hours ago
0 STEP 2
1 23105U 94029A   26119.03887867  .00003608  00000-0  34348-3 0  9993
2 23105  81.9395 224.0206 0083511  61.4137 299.5450 14.90493074712560
Epoch: 2026-04-29T00:55Z
TLE epoch observation values (Epoch: 2026-04-29T00:55:59.117Z)
Latitude
-0.00005°
Longitude
-6.9813°
Altitude
571.071 km
Speed
7.591 km/s
True Right ascension
14h 56m 04s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
15:16:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.651 km
Perigee altitude
535.211 km
Semi-major axis
6,971.568 km
Eccentricity
0.00835
Inclination
81.9395°
RAAN
224.0206°
Arg. of periapsis
61.4137°
True anomaly
298.70819°
Mean anomaly
299.545°
Eccentric anomaly
299.12702°
Mean motion
3.72861 °/min
Orbital period
96.55 mins
BSTAR
0.00034348
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|