SL-16 R/B, 22566

Orbit data source: Space-Track

SL-16 R/B, 22566 is space debris in LEO originally from a launch on Fri, 26 Mar 1993 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
22566, 1993-016B
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Yuzhnoe
Mission
Spacecraft
Bus & Motor
11S772, Unknown motor
Mass
9,000 kg wet, 9,000 kg dry
Launch date (UTC)
1993-03-26 (33 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 5.2 m
Radar Cross Section
37.829 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 SL-16 R/B
1 22566U 93016B   25307.90277792 -.00000177  00000-0 -66608-4 0  9997
2 22566  71.0049 119.3694 0009497 167.9628 192.1724 14.15278665684374
Epoch: 2025-11-03T21:40Z
TLE epoch observation values (Epoch: 2025-11-03T21:40:00.012Z)
Latitude
0.00003°
Longitude
110.97188°
Altitude
850.469 km
Speed
7.424 km/s
True Right ascension
07h 57m 28s
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
06:56:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
846.143 km
Perigee altitude
832.434 km
Semi-major axis
7,217.425 km
Eccentricity
0.00095
Inclination
71.0049°
RAAN
119.3694°
Arg. of periapsis
167.9628°
True anomaly
192.14948°
Mean anomaly
192.1724°
Eccentric anomaly
192.16094°
Mean motion
3.53973 °/min
Orbital period
101.7 mins
BSTAR
-0.000066608
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