SL-12 R/B(2), 19754

Orbit data source: Space-Track

SL-12 R/B(2), 19754 is space debris in MEO originally from a launch on Tue, 10 Jan 1989 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
19754, 1989-001F
Orbit
MEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO Energiya
Mission
Spacecraft
Bus & Motor
BLOK DM, Unknown motor
Mass
2,440 kg wet, 2,440 kg dry
Launch date (UTC)
1989-01-10 (37 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.1 m
Radar Cross Section
23.597 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(2)
1 19754U 89001F   26171.19247873 -.00000042  00000-0  00000-0 0  9999
2 19754  64.9688  70.6994 0015534 238.0296 314.4010  2.13421130291767
Epoch: 2026-06-20T04:37Z
TLE epoch observation values (Epoch: 2026-06-20T04:37:10.162Z)
Latitude
-11.17052°
Longitude
-81.71317°
Altitude
19,079.524 km
Speed
3.959 km/s
True Right ascension
17h 03m 57s
True Declination
-11° 09' 08"
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
00:51:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,143.653 km
Perigee altitude
19,064.484 km
Semi-major axis
25,482.205 km
Eccentricity
0.00155
Inclination
64.9688°
RAAN
70.6994°
Arg. of periapsis
238.0296°
True anomaly
314.27365°
Mean anomaly
314.401°
Eccentric anomaly
314.33734°
Mean motion
0.53357 °/min
Orbital period
674.71 mins
BSTAR
0
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