ANTELSAT, 40034
Orbit data source: Space-Track
ANTELSAT, 40034 is an Uruguayan payload satellite in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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40034 intel report (Beta)
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ANTELSAT radio frequencies
ANTELSAT details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 14 hours ago |
| Origin | |
| Manufacturer | UdelaR FING |
| Mission | Non-operational Civil Tech/Com |
| Bus & Motor | CUBESAT 2U, Unknown motor |
| Mass | ~2 kg wet, ~2 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Ant, 0.2 m |
| Radar Cross Section | 0.040 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 14 hours ago
0 ANTELSAT
1 40034U 14033AA 24361.01023043 .00007829 00000-0 91323-3 0 9998
2 40034 97.7131 158.1019 0049525 33.8876 326.5487 14.84567783565774Epoch: 2024-12-26T00:14Z
Definitive object data (Epoch: 2024-12-26T00:14:43.909Z)
| Latitude | 0.00005° |
| Longitude | 59.42317° |
| Altitude | 589.126 km |
| Speed | 7.581 km/s |
| True Right ascension | 10h 32m 24s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -22.01943° |
| Longitude | -123.1416° |
| Altitude | 657.393 km |
| Speed | 7.509 km/s |
| Apparent Right ascension | 23h 40m 47s |
| Apparent Declination | -32° 27' 30" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:27:17 |
| Azimuth | 79.163° E |
| Elevation | -67.356° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 646.588 km |
| Perigee altitude | 577.351 km |
| Semi-major axis | 6,990.106 km |
| Eccentricity | 0.0049525 |
| Inclination | 97.7131° |
| RAAN | 158.1019° |
| Arg. of periapsis | 33.8876° |
| True anomaly | 326.23425° |
| Mean anomaly | 326.5487° |
| Eccentric anomaly | 326.39164° |
| Mean motion | 3.71379 °/min |
| BSTAR | 0.00091323 |
| Orbital period | 96.94 mins |
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Other satellites on launch #33 in the year 2014 (2014-06-19 UTC)
ANTELSAT 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-12-26 23:27:30.214Z | 17.451° NNE | 2024-12-26 23:31:30.214Z | 153.51° SSE | 42.176° | 2024-12-26 23:34:30.214Z | 185.914° SSW |
| 7 mins | 2024-12-27 10:20:30.214Z | 145.053° SSE | 2024-12-27 10:23:30.214Z | 95.156° ESE | 35.208° | 2024-12-27 10:27:30.214Z | 1.412° NNE |
Authenticating...
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