SL-14 R/B, 20466

Orbit data source: Space-Track

SL-14 R/B, 20466 is space debris in LEO originally from a launch on Tue, 30 Jan 1990 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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
20466, 1990-010B
Orbit
LEO
Last TLE update
11 hours ago
Origin
Manufacturer
Yuzhnoe
Mission
Spacecraft
Bus & Motor
S5M, Unknown motor
Mass
1,600 kg wet, 1,600 kg dry
Launch date (UTC)
1990-01-30 (35 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
7.351 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 11 hours ago
0 SL-14 R/B
1 20466U 90010B   25203.87430759  .00000407  00000-0  46726-4 0  9993
2 20466  82.5038 123.1888 0019404 341.7928  18.2590 14.83286647915479
Epoch: 2025-07-22T20:59Z
TLE epoch observation values (Epoch: 2025-07-22T20:59:00.175Z)
Latitude
-0°
Longitude
-132.42403°
Altitude
609.113 km
Speed
7.562 km/s
True Right ascension
08h 12m 45s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-18.34956°
Longitude
-135.35175°
Altitude
612.569 km
Speed
7.559 km/s
Apparent Right ascension
08h 34m 02s
Apparent Declination
-28° 49' 23"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
21:18:52
Azimuth
43.147° NE
Elevation
-75.581°
Doppler factor
1
Orbital elements
Apogee altitude
629.559 km
Perigee altitude
602.416 km
Semi-major axis
6,994.125 km
Eccentricity
0.00194
Inclination
82.5038°
RAAN
123.1888°
Arg. of periapsis
341.7928°
True anomaly
18.32883°
Mean anomaly
18.259°
Eccentric anomaly
18.2939°
Mean motion
3.71059 °/min
Orbital period
97.02 mins
BSTAR
0.000046726
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Other satellites on launch #10 in the year 1990 (1990-01-30 UTC)
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