OBJECT C, 60205
Orbit data source: Space-Track
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, 60205 is a satellite owned by Teachers in Space (US) in SSO that was launched on Thu, 04 Jul 2024 UTC via an FIREFLY ALPHA launch vehicle from the Air Force Western Test Range (AFWTR). 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.
60205 intel report (Beta)
OBJECT C radio frequencies
OBJECT C details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | Quub |
| Mission | Operational spacecraft |
| 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 | Unknown |
| Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 OBJECT C
1 60205U 24125C 24355.52571527 .00026999 00000-0 91856-3 0 9997
2 60205 97.2963 204.3945 0019878 21.4516 338.7554 15.30211020 25805Definitive object data (Epoch: 2024-12-20T12:37:01.799Z)
| Latitude | 0.00003° |
| Longitude | -74.45297° |
| Altitude | 465.593 km |
| Speed | 7.641 km/s |
| True Right ascension | 13h 37m 34s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 48.10981° |
| Longitude | 114.82387° |
| Altitude | 488.131 km |
| Speed | 7.623 km/s |
| Apparent Right ascension | 02h 35m 12s |
| Apparent Declination | 6° 08' 32" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 14:54:27 |
| Azimuth | 6.626° NNE |
| Elevation | -43.728° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 485.747 km |
| Perigee altitude | 458.513 km |
| Semi-major axis | 6,850.267 km |
| Eccentricity | 0.0019878 |
| Inclination | 97.2963° |
| RAAN | 204.3945° |
| Arg. of periapsis | 21.4516° |
| True anomaly | 338.67267° |
| Mean anomaly | 338.7554° |
| Eccentric anomaly | 338.71405° |
| Mean motion | 3.82809 °/min |
| BSTAR | 0.00091856 |
| Orbital period | 94.04 mins |
Other satellites on launch #125 in the year 2024 (2024-07-04 UTC)
| OBJECT A, 60203 |
| OBJECT B, 60204 |
| OBJECT C, 60205 |
| R5-S4, 60206 |
| R5-S2, 60207 |
| TECHEDSAT-11, 60208 |
| OBJECT G, 60209 |
| FIREFLY ALPHA R/B, 60210 |
| CATSAT, 60246 |
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-12-22 02:50:05.497Z | 18.776° NNE | 2024-12-22 02:53:05.497Z | 64.191° ENE | 40.172° | 2024-12-22 02:56:05.497Z | 179.685° S |
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