SL-12 R/B(AUX MOTOR), 21220

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 21220 is space debris in HEO originally from a launch on Thu, 04 Apr 1991 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
21220, 1991-025F
Orbit
HEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO Energiya
Mission
Spacecraft
Bus & Motor
SOZ, Unknown motor
Mass
Wet unknown, ~60 kg dry
Launch date (UTC)
1991-04-04 (35 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.6 m
Radar Cross Section
0.660 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 SL-12 R/B(AUX MOTOR)
1 21220U 91025F   26171.29951416  .00000047  00000-0  30758-3 0  9995
2 21220  65.1125 233.1429 5506926 116.8381 308.9508  4.44046146551001
Epoch: 2026-06-20T07:11Z
TLE epoch observation values (Epoch: 2026-06-20T07:11:18.023Z)
Latitude
-0.00003°
Longitude
-143.19539°
Altitude
8,114.546 km
Speed
5.433 km/s
True Right ascension
15h 32m 34s
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
23:09:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
17,866.232 km
Perigee altitude
646.579 km
Semi-major axis
15,634.543 km
Eccentricity
0.55069
Inclination
65.1125°
RAAN
233.1429°
Arg. of periapsis
116.8381°
True anomaly
243.24597°
Mean anomaly
308.9508°
Eccentric anomaly
277.68158°
Mean motion
1.11024 °/min
Orbital period
324.26 mins
BSTAR
0.00030758
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