OBJECT F, 57429
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 F, 57429 is a Chinese satellite in SSO that was launched on Sun, 23 Jul 2023 UTC via a CHANG ZHENG 2D launch vehicle from the Taiyaun Space Center, China (TSC). 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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57429 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
16.383 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 OBJECT F
1 57429U 23104F 25308.27163102 .00024423 00000-0 56599-3 0 9999
2 57429 97.2890 15.9993 0024559 137.4513 222.8643 15.42095228127688Epoch: 2025-11-04T06:31Z
TLE epoch observation values (Epoch: 2025-11-04T06:31:08.920Z)
Latitude
-0.00003°
Longitude
-125.54891°
Altitude
455.345 km
Speed
7.632 km/s
True Right ascension
01h 03m 59s
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
08:42:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.595 km
Perigee altitude
420.121 km
Semi-major axis
6,814.995 km
Eccentricity
0.00246
Inclination
97.289°
RAAN
15.9993°
Arg. of periapsis
137.4513°
True anomaly
222.67329°
Mean anomaly
222.8643°
Eccentric anomaly
222.76875°
Mean motion
3.85785 °/min
Orbital period
93.32 mins
BSTAR
0.00056599
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Other satellites on launch #104 in the year 2023 (2023-07-23 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 F 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 | 2025-11-04 17:59:07.626Z | 342.654° N | 2025-11-04 18:01:07.626Z | 283.821° WNW | 28.778° | 2025-11-04 18:03:07.626Z | 228.927° WSW |
| 4 mins | 2025-11-05 04:28:07.626Z | 143.066° SSE | 2025-11-05 04:30:07.626Z | 59.733° ENE | 37.851° | 2025-11-05 04:32:07.626Z | 3.818° NNE |
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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