CZ-2D R/B, 36597

Orbit data source: Space-Track

CZ-2D R/B, 36597 is space debris in SSO originally from a launch on Tue, 15 Jun 2010 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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
36597, 2010-027B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
BWYIC
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
4,006 kg wet, 4,006 kg dry
Launch date (UTC)
2010-06-15 (16 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Sail, 4.0 m
Radar Cross Section
25.456 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 hours ago

TLE from 4 hours ago
0 CZ-2D R/B
1 36597U 10027B   26080.58153820  .00001532  00000-0  11796-3 0  9996
2 36597  97.9877 107.1768 0048454 212.0613 147.7661 15.02379984857728
Epoch: 2026-03-21T13:57Z
TLE epoch observation values (Epoch: 2026-03-21T13:57:24.900Z)
Latitude
-0.00008°
Longitude
78.72287°
Altitude
591.096 km
Speed
7.549 km/s
True Right ascension
07h 08m 42s
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
22:45:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.176 km
Perigee altitude
522.973 km
Semi-major axis
6,934.712 km
Eccentricity
0.00485
Inclination
97.9877°
RAAN
107.1768°
Arg. of periapsis
212.0613°
True anomaly
148.06074°
Mean anomaly
147.7661°
Eccentric anomaly
147.91357°
Mean motion
3.75838 °/min
Orbital period
95.79 mins
BSTAR
0.00011796
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