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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36597 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated 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)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 4.0 m
Radar Cross Section
25.456 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 CZ-2D R/B
1 36597U 10027B 26126.06749538 .00002462 00000-0 18455-3 0 9999
2 36597 97.9826 154.0233 0051671 63.2091 297.4406 15.02623054864550Epoch: 2026-05-06T01:37Z
TLE epoch observation values (Epoch: 2026-05-06T01:37:11.600Z)
Latitude
0.00003°
Longitude
-94.20834°
Altitude
545.486 km
Speed
7.598 km/s
True Right ascension
10h 16m 05s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
22:35:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.654 km
Perigee altitude
519.997 km
Semi-major axis
6,933.963 km
Eccentricity
0.00517
Inclination
97.9826°
RAAN
154.0233°
Arg. of periapsis
63.2091°
True anomaly
296.91355°
Mean anomaly
297.4406°
Eccentric anomaly
297.17723°
Mean motion
3.75899 °/min
Orbital period
95.77 mins
BSTAR
0.00018455
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Other satellites on launch #27 in the year 2010 (2010-06-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-2D R/B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-06 14:58:04.010Z | 2.582° NNE | 2026-05-06 15:01:04.010Z | 281.471° WNW | 41.201° | 2026-05-06 15:04:04.010Z | 207.769° SW |
| 5 mins | 2026-05-07 01:44:04.010Z | 155.475° SSE | 2026-05-07 01:46:04.010Z | 106.785° ESE | 42.9° | 2026-05-07 01:49:04.010Z | 353.807° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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