TDS 1, 40076
Orbit data source: Space-Track
TDS 1, 40076 is a payload satellite owned by UK TSB (UK) in SSO that was launched on Tue, 08 Jul 2014 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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40076 intel report (Beta)
TDS 1 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 10 hours ago |
| Origin | |
| Manufacturer | SSTL (Astrium) |
| Mission | Partially operational Civil Technology |
| Bus & Motor | SSTL-150, AOCS |
| Mass | 157 kg wet, 157 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, 1 m |
| Radar Cross Section | 1.500 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 TDS 1
1 40076U 14037H 24361.06909944 .00015617 00000-0 12336-2 0 9996
2 40076 98.3297 296.0509 0004388 267.3890 92.6830 15.00776572567237Epoch: 2024-12-26T01:39Z
Definitive object data (Epoch: 2024-12-26T01:39:30.191Z)
| Latitude | 0° |
| Longitude | 176.12131° |
| Altitude | 567.681 km |
| Speed | 7.577 km/s |
| True Right ascension | 19h 44m 12s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -4.84994° |
| Longitude | 177.25672° |
| Altitude | 568.211 km |
| Speed | 7.577 km/s |
| Apparent Right ascension | 20h 57m 14s |
| Apparent Declination | -22° 48' 22" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 10:35:34 |
| Azimuth | 57.897° ENE |
| Elevation | -63.082° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 564.579 km |
| Perigee altitude | 558.488 km |
| Semi-major axis | 6,939.67 km |
| Eccentricity | 0.0004388 |
| Inclination | 98.3297° |
| RAAN | 296.0509° |
| Arg. of periapsis | 267.389° |
| True anomaly | 92.73323° |
| Mean anomaly | 92.683° |
| Eccentric anomaly | 92.70811° |
| Mean motion | 3.75435 °/min |
| BSTAR | 0.0012336 |
| Orbital period | 95.89 mins |
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Other satellites on launch #37 in the year 2014 (2014-07-08 UTC)
| METEOR M2, 40069 |
| MKA PN2 (RELEK), 40070 |
| DX 1, 40071 |
| SKYSAT 2, 40072 |
| DUMMY SAT, 40073 |
| UKUBE 1, 40074 |
| AISSAT 2, 40075 |
| TDS 1, 40076 |
| SL-4 R/B, 40077 (Decayed) |
| FREGAT DEB, 40078 |
TDS 1 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 19:23:15.412Z | 138.708° SSE | 2024-12-26 19:27:15.412Z | 53.276° ENE | 30.914° | 2024-12-26 19:30:15.412Z | 4.52° NNE |
| 6 mins | 2024-12-27 08:38:15.412Z | 23.538° NE | 2024-12-27 08:41:15.412Z | 124.829° SE | 41.444° | 2024-12-27 08:44:15.412Z | 182.05° SSW |
Authenticating...
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