OBJECT G, 44316
Orbit data source: Space-Track
OBJECT G, 44316 is a Chinese payload satellite in LEO that was launched on Wed, 05 Jun 2019 UTC via a CHANG ZHENG 11 launch vehicle from the Yellow Sea Launch Area, China (YSLA). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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44316 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.9 m
Radar Cross Section
1.500 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 hours ago
TLE from 3 hours ago
0 OBJECT G
1 44316U 19032G 26317.98933361 .00016628 00000-0 57012-3 0 9995
2 44316 44.9730 321.5673 0010317 33.5504 326.6031 15.29992093410001Epoch: 2026-11-13T23:44Z
TLE epoch observation values (Epoch: 2026-11-13T23:44:38.423Z)
Latitude
-0.00005°
Longitude
-87.69341°
Altitude
469.931 km
Speed
7.636 km/s
True Right ascension
21h 26m 16s
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
23:22:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.524 km
Perigee altitude
470.378 km
Semi-major axis
6,855.588 km
Eccentricity
0.00103
Inclination
44.973°
RAAN
321.5673°
Arg. of periapsis
33.5504°
True anomaly
326.53796°
Mean anomaly
326.6031°
Eccentric anomaly
326.57053°
Mean motion
3.82363 °/min
Orbital period
94.15 mins
BSTAR
0.00057012
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Other satellites on launch #32 in the year 2019 (2019-06-05 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 G 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 | 2026-11-14 03:03:35.071Z | 183.589° SSW | 2026-11-14 03:05:35.071Z | 144.381° SSE | 20.789° | 2026-11-14 03:07:35.071Z | 102.955° ESE |
| 6 mins | 2026-11-14 04:41:35.071Z | 251.423° W | 2026-11-14 04:43:35.071Z | 271.23° WNW | 66.492° | 2026-11-14 04:47:35.071Z | 65.005° ENE |
| 5 mins | 2026-11-14 06:20:35.071Z | 295.349° NW | 2026-11-14 06:22:35.071Z | 341.339° N | 35.803° | 2026-11-14 06:25:35.071Z | 58.677° ENE |
| 6 mins | 2026-11-14 07:59:35.071Z | 305.16° NW | 2026-11-14 08:01:35.071Z | 350.694° N | 45.52° | 2026-11-14 08:05:35.071Z | 90.082° ESE |
| 5 mins | 2026-11-14 09:38:35.071Z | 275.253° WNW | 2026-11-14 09:40:35.071Z | 214.471° SW | 46.867° | 2026-11-14 09:43:35.071Z | 139.943° 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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