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
CALT
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, 4.3 m
Radar Cross Section
25.456 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 CZ-2D R/B
1 36597U 10027B   26307.55550485  .00000947  00000-0  73068-4 0  9993
2 36597  97.9669 340.8626 0049357 170.0820 190.1390 15.03267453891819
Epoch: 2026-11-03T13:19Z
TLE epoch observation values (Epoch: 2026-11-03T13:19:55.619Z)
Latitude
-0.00006°
Longitude
98.06438°
Altitude
593.587 km
Speed
7.545 km/s
True Right ascension
22h 43m 27s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
16:28:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.056 km
Perigee altitude
519.628 km
Semi-major axis
6,931.979 km
Eccentricity
0.00494
Inclination
97.9669°
RAAN
340.8626°
Arg. of periapsis
170.082°
True anomaly
190.04004°
Mean anomaly
190.139°
Eccentric anomaly
190.08946°
Mean motion
3.7606 °/min
Orbital period
95.73 mins
BSTAR
0.000073068
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