OBJECT C, 62265
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 C, 62265 is a satellite owned by IRSA (IR) in LEO that was launched on Fri, 06 Dec 2024 UTC via an SIMORGH launch vehicle from the Semnan, Iran (SEM). 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.
Focus sentinelFocus sentinel
62265 intel report (Beta)
OBJECT C details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 4 days ago |
| Origin | |
| Manufacturer | IEI |
| Mission | Decayed spacecraft |
| Bus & Motor | FAKHR, Unknown motor |
| Mass | 5 kg wet, 5 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Unknown |
| Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 4 days ago
0 OBJECT C
1 62265U 24236C 25021.46258119 .08699274 10950-4 67855-3 0 9992
2 62265 58.5427 179.2943 0014353 266.2054 93.7422 16.39187091 7357Epoch: 2025-01-21T11:06Z
Definitive object data (Epoch: 2025-01-21T11:06:07.014Z)
| Latitude | -0.00003° |
| Longitude | -108.3034° |
| Altitude | 170.12 km |
| Speed | 7.805 km/s |
| True Right ascension | 11h 57m 10s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 176.749 km |
| Perigee altitude | 157.96 km |
| Semi-major axis | 6,545.491 km |
| Eccentricity | 0.0014353 |
| Inclination | 58.5427° |
| RAAN | 179.2943° |
| Arg. of periapsis | 266.2054° |
| True anomaly | 93.9063° |
| Mean anomaly | 93.7422° |
| Eccentric anomaly | 93.82425° |
| Mean motion | 4.09855 °/min |
| BSTAR | 0.00067855 |
| Orbital period | 87.84 mins |
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #236 in the year 2024 (2024-12-06 UTC)
| OBJECT A, 62263 |
| OBJECT B, 62264 |
| OBJECT C, 62265 |
| OBJECT D, 62266 |
OBJECT C Visibility forecast
Observer location: undefined°, undefined
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. |
|---|
Authenticating...
Click to sort rows by NORAD ID header in ascending order | Click to sort rows by Common name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
|---|