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 (38 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.6 m
Radar Cross Section
23.597 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 SL-12 R/B(2)
1 19754U 89001F   26254.12524590  .00000005  00000-0  00000-0 0  9996
2 19754  65.0229  67.8590 0015530 234.4702 316.3182  2.13421215293530
Epoch: 2026-09-11T03:00Z
TLE epoch observation values (Epoch: 2026-09-11T03:00:21.245Z)
Latitude
-9.69476°
Longitude
-142.83175°
Altitude
19,078.314 km
Speed
3.959 km/s
True Right ascension
16h 49m 38s
True Declination
-9° 40' 44"
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
04:28:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,143.634 km
Perigee altitude
19,064.486 km
Semi-major axis
25,482.197 km
Eccentricity
0.00155
Inclination
65.0229°
RAAN
67.859°
Arg. of periapsis
234.4702°
True anomaly
316.19512°
Mean anomaly
316.3182°
Eccentric anomaly
316.25668°
Mean motion
0.53357 °/min
Orbital period
674.71 mins
BSTAR
0
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