OBJECT F, 65549
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, 65549 is a satellite owned by CNSA (CN) in LEO that was launched on Sat, 06 Sep 2025 UTC launched 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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65549 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-6A STAGE 2, YF-115
Mass
~6,000 kg wet, ~6,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 OBJECT F
1 65549U 25199F 25260.19494372 .00000487 00000-0 84909-4 0 9992
2 65549 86.0173 166.3027 0069770 35.5813 325.0021 14.64053574 1536Epoch: 2025-09-17T04:40Z
TLE epoch observation values (Epoch: 2025-09-17T04:40:43.137Z)
Latitude
0.00002°
Longitude
99.74858°
Altitude
642.968 km
Speed
7.558 km/s
True Right ascension
11h 05m 12s
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
12:32:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
726.27 km
Perigee altitude
627.822 km
Semi-major axis
7,055.183 km
Eccentricity
0.00698
Inclination
86.0173°
RAAN
166.3027°
Arg. of periapsis
35.5813°
True anomaly
324.54025°
Mean anomaly
325.0021°
Eccentric anomaly
324.77151°
Mean motion
3.66253 °/min
Orbital period
98.29 mins
BSTAR
0.000084909
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Other satellites on launch #199 in the year 2025 (2025-09-06 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 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-18 05:50:38.240Z | 0.094° NNE | 2025-09-18 05:54:38.240Z | 44.607° NE | 44.027° | 2025-09-18 05:59:38.240Z | 174.012° S |
| 6 mins | 2025-09-18 18:32:38.240Z | 196.079° SSW | 2025-09-18 18:35:38.240Z | 313.417° NW | 41.475° | 2025-09-18 18:38:38.240Z | 355.451° 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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