CZ-2D DEB, 44607
Orbit data source: Space-Track
CZ-2D DEB, 44607 is space debris in SSO originally from a launch on Fri, 11 Nov 2016 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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44607 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CZ-2D DEB
1 44607U 16068G 25307.19173806 .00000873 00000-0 55082-3 0 9995
2 44607 98.4901 92.6131 0205186 81.0904 281.3427 13.96560927449282Epoch: 2025-11-03T04:36Z
TLE epoch observation values (Epoch: 2025-11-03T04:36:06.168Z)
Latitude
-0.00004°
Longitude
-19.10924°
Altitude
882.185 km
Speed
7.425 km/s
True Right ascension
06h 10m 27s
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
06:56:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,052.303 km
Perigee altitude
753.51 km
Semi-major axis
7,281.043 km
Eccentricity
0.02052
Inclination
98.4901°
RAAN
92.6131°
Arg. of periapsis
81.0904°
True anomaly
279.02631°
Mean anomaly
281.3427°
Eccentric anomaly
280.1856°
Mean motion
3.49344 °/min
Orbital period
103.05 mins
BSTAR
0.00055082
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Other satellites on launch #68 in the year 2016 (2016-11-11 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 DEB 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-04 22:26:03.416Z | 20.488° NNE | 2025-11-04 22:31:03.416Z | 103.185° ESE | 41.824° | 2025-11-04 22:36:03.416Z | 182.078° SSW |
| 4 mins | 2025-11-05 00:11:03.416Z | 315.485° NNW | 2025-11-05 00:12:03.416Z | 302.307° NW | 15.894° | 2025-11-05 00:15:03.416Z | 265.334° W |
| 8 mins | 2025-11-05 10:02:03.416Z | 180.223° SSW | 2025-11-05 10:05:03.416Z | 233.855° WSW | 42.002° | 2025-11-05 10:10:03.416Z | 340.222° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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