CZ-3 R/B, 20559

Orbit data source: Space-Track

CZ-3 R/B, 20559 is space debris originally from a launch on Sat, 07 Apr 1990 UTC launched from the Xichang Space Center, China (XSC). 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
20559, 1990-030B
Orbit
Active
Last TLE update
17 hours ago
Origin
Manufacturer
BWYIC
Mission
Spacecraft
Bus & Motor
CZ-3 STAGE 3, Unknown motor
Mass
~2,000 kg wet, ~2,000 kg dry
Launch date (UTC)
1990-04-07 (35 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.7 m
Radar Cross Section
15.189 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 17 hours ago
0 CZ-3 R/B
1 20559U 90030B   25224.08346561  .00113299  61468-7  14343-2 0  9995
2 20559  30.7781 233.9764 4315671  74.2248 328.2633  6.97662876226528
Epoch: 2025-08-12T02:00Z
TLE epoch observation values (Epoch: 2025-08-12T02:00:11.428Z)
Latitude
-0.00002°
Longitude
-116.85245°
Altitude
2,043.409 km
Speed
7.76 km/s
True Right ascension
15h 35m 54s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
6.93873°
Longitude
-106.28114°
Altitude
1,465.427 km
Speed
8.197 km/s
Apparent Right ascension
18h 15m 53s
Apparent Declination
-17° 38' 01"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
09:41:15
Azimuth
78.63° E
Elevation
-40.615°
Doppler factor
1
Orbital elements
Apogee altitude
10,188.523 km
Perigee altitude
199.993 km
Semi-major axis
11,572.395 km
Eccentricity
0.43157
Inclination
30.7781°
RAAN
233.9764°
Arg. of periapsis
74.2248°
True anomaly
285.83248°
Mean anomaly
328.2633°
Eccentric anomaly
309.06431°
Mean motion
1.74345 °/min
Orbital period
206.49 mins
BSTAR
0.0014343
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