OBJECT P, 61748
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 P, 61748 is a satellite in SSO that was launched on Mon, 04 Nov 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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61748 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
Manufacturer
Sputniks
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 OBJECT P
1 61748U 24199P 25361.30837009 .00042597 00000-0 80866-3 0 9996
2 61748 97.3197 231.1853 0006603 165.1981 194.9464 15.48154209111035Epoch: 2025-12-27T07:24Z
TLE epoch observation values (Epoch: 2025-12-27T07:24:03.175Z)
Latitude
-0.00005°
Longitude
24.13551°
Altitude
429.596 km
Speed
7.651 km/s
True Right ascension
15h 24m 44s
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
12:01:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
423.539 km
Perigee altitude
414.562 km
Semi-major axis
6,797.187 km
Eccentricity
0.00066
Inclination
97.3197°
RAAN
231.1853°
Arg. of periapsis
165.1981°
True anomaly
194.9269°
Mean anomaly
194.9464°
Eccentric anomaly
194.93665°
Mean motion
3.87302 °/min
Orbital period
92.95 mins
BSTAR
0.00080866
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Other satellites on launch #199 in the year 2024 (2024-11-04 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 P 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-27 15:17:34.060Z | 146.873° SSE | 2025-12-27 15:19:34.060Z | 104.525° ESE | 34.908° | 2025-12-27 15:22:34.060Z | 2.594° NNE |
| 4 mins | 2025-12-28 04:08:34.060Z | 33.933° NE | 2025-12-28 04:10:34.060Z | 123.778° SE | 36.105° | 2025-12-28 04:12:34.060Z | 172.413° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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