OBJECT A, 44310
Orbit data source: Space-Track
OBJECT A, 44310 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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44310 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: 4 hours ago
TLE from 4 hours ago
0 OBJECT A
1 44310U 19032A 26317.95135281 .00017143 00000-0 56562-3 0 9993
2 44310 44.9704 316.1560 0010031 43.0868 317.0800 15.31218182410127Epoch: 2026-11-13T22:49Z
TLE epoch observation values (Epoch: 2026-11-13T22:49:56.882Z)
Latitude
-0.00001°
Longitude
-79.39414°
Altitude
467.144 km
Speed
7.637 km/s
True Right ascension
21h 04m 37s
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
23:34:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.667 km
Perigee altitude
466.92 km
Semi-major axis
6,851.93 km
Eccentricity
0.001
Inclination
44.9704°
RAAN
316.156°
Arg. of periapsis
43.0868°
True anomaly
317.00165°
Mean anomaly
317.08°
Eccentric anomaly
317.04083°
Mean motion
3.82669 °/min
Orbital period
94.08 mins
BSTAR
0.00056562
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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 A 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 | 2026-11-14 03:44:38.231Z | 230.094° WSW | 2026-11-14 03:47:38.231Z | 138.027° SSE | 61.149° | 2026-11-14 03:50:38.231Z | 72.187° E |
| 5 mins | 2026-11-14 05:24:38.231Z | 295.427° NW | 2026-11-14 05:26:38.231Z | 11.847° NNE | 39.835° | 2026-11-14 05:29:38.231Z | 61.721° ENE |
| 5 mins | 2026-11-14 07:03:38.231Z | 317.601° NNW | 2026-11-14 07:05:38.231Z | 28.165° NE | 36.665° | 2026-11-14 07:08:38.231Z | 78.265° E |
| 5 mins | 2026-11-14 08:41:38.231Z | 291.228° WNW | 2026-11-14 08:43:38.231Z | 266.612° W | 73.449° | 2026-11-14 08:46:38.231Z | 119.074° SE |
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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