CZ-2D DEB, 44609
Orbit data source: Space-Track
CZ-2D DEB, 44609 is space debris in SSO originally from a launch on Mon, 09 Oct 2017 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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44609 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: 18 hours ago
TLE from 18 hours ago
0 CZ-2D DEB
1 44609U 17060B 25298.31110308 .00007972 00000-0 68155-3 0 9993
2 44609 97.5523 319.2000 0033617 23.5400 336.7352 14.97447577429992Epoch: 2025-10-25T07:27Z
TLE epoch observation values (Epoch: 2025-10-25T07:27:59.306Z)
Latitude
-0.00001°
Longitude
173.25942°
Altitude
556.376 km
Speed
7.595 km/s
True Right ascension
21h 16m 48s
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
20:55:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.152 km
Perigee altitude
548.425 km
Semi-major axis
6,949.925 km
Eccentricity
0.00336
Inclination
97.5523°
RAAN
319.2°
Arg. of periapsis
23.54°
True anomaly
336.58245°
Mean anomaly
336.7352°
Eccentric anomaly
336.65889°
Mean motion
3.74604 °/min
Orbital period
96.1 mins
BSTAR
0.00068155
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Other satellites on launch #60 in the year 2017 (2017-10-09 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-26 14:30:47.144Z | 6.071° NNE | 2025-10-26 14:33:47.144Z | 228.626° WSW | 42.375° | 2025-10-26 14:36:47.144Z | 199.555° SSW |
| 5 mins | 2025-10-27 01:18:47.144Z | 142.426° SSE | 2025-10-27 01:20:47.144Z | 63.739° ENE | 39.948° | 2025-10-27 01:23:47.144Z | 358.727° 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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