OBJECT D, 60015
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT D, 60015 is a satellite owned by Xinghe Dongli (CN) in SSO that was launched on Thu, 06 Jun 2024 UTC via a GUSHENXING 1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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60015 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Xinghe Dongli
Mission
Spacecraft
Bus & Motor
LSP, EDGE
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 OBJECT D
1 60015U 24110D 25259.55564449 .00009978 00000-0 48871-3 0 9999
2 60015 97.5806 349.9169 0012682 125.6341 234.6075 15.18296243 70646Epoch: 2025-09-16T13:20Z
TLE epoch observation values (Epoch: 2025-09-16T13:20:07.683Z)
Latitude
-0.00013°
Longitude
154.14065°
Altitude
519.141 km
Speed
7.601 km/s
True Right ascension
23h 19m 40s
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
18:26:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.698 km
Perigee altitude
499.232 km
Semi-major axis
6,886.102 km
Eccentricity
0.00127
Inclination
97.5806°
RAAN
349.9169°
Arg. of periapsis
125.6341°
True anomaly
234.48914°
Mean anomaly
234.6075°
Eccentric anomaly
234.54831°
Mean motion
3.79824 °/min
Orbital period
94.78 mins
BSTAR
0.00048871
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Other satellites on launch #110 in the year 2024 (2024-06-06 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.OBJECT D 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-17 05:18:37.747Z | 106.337° ESE | 2025-09-17 05:20:37.747Z | 66.35° ENE | 18.89° | 2025-09-17 05:22:37.747Z | 28.407° NE |
| 4 mins | 2025-09-17 06:52:37.747Z | 225.138° WSW | 2025-09-17 06:54:37.747Z | 272.387° WNW | 22.219° | 2025-09-17 06:56:37.747Z | 311.996° NW |
| 4 mins | 2025-09-17 18:23:37.747Z | 52.134° ENE | 2025-09-17 18:25:37.747Z | 102.735° ESE | 24.964° | 2025-09-17 18:27:37.747Z | 147.121° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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