EUTE 21A (EUTE W3), 25673
Orbit data source: Space-Track
EUTE 21A (EUTE W3), 25673 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Mon, 12 Apr 1999 UTC via an ATLAS IIAS launch vehicle from the Air Force Eastern Test Range (AFETR). 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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25673 intel report (Beta)
EUTE 21A (EUTE W3) details
| Identifier | |
| Orbit | GEO |
| Last TLE update | 14 hours ago |
| Origin | |
| Manufacturer | Alcatel/Cannes |
| Mission | Non-operational Civil Communications |
| Bus & Motor | SPACEBUS 3000B2, S400 |
| Mass | 3,177 kg wet, 1,380 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, Unknown HBR |
| Radar Cross Section | 32.393 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 14 hours ago
0 EUTE 21A (EUTE W3)
1 25673U 99018A 24360.95031214 -.00000164 00000-0 00000-0 0 9992
2 25673 9.3447 55.5965 0004961 113.9924 229.8074 0.98431149 36253Epoch: 2024-12-25T22:48Z
Definitive object data (Epoch: 2024-12-25T22:48:26.968Z)
| Latitude | -2.59957° |
| Longitude | -37.49537° |
| Altitude | 36,324.108 km |
| Speed | 3.055 km/s |
| True Right ascension | 02h 38m 12s |
| True Declination | -2° 35' 49" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -1.06366° |
| Longitude | 164.93204° |
| Altitude | 36,304.014 km |
| Speed | 3.056 km/s |
| Apparent Right ascension | 16h 32m 40s |
| Apparent Declination | -6° 48' 24" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:53:20 |
| Azimuth | 108.429° ESE |
| Elevation | 10.751° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 36,332.812 km |
| Perigee altitude | 36,290.455 km |
| Semi-major axis | 42,689.77 km |
| Eccentricity | 0.0004961 |
| Inclination | 9.3447° |
| RAAN | 55.5965° |
| Arg. of periapsis | 113.9924° |
| True anomaly | 229.76399° |
| Mean anomaly | 229.8074° |
| Eccentric anomaly | 229.78569° |
| Mean motion | 0.24607 °/min |
| BSTAR | Unknown |
| Orbital period | 1463 mins |
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25673 neighbors
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Other satellites on launch #18 in the year 1999 (1999-04-12 UTC)
| EUTE 21A (EUTE W3), 25673 |
| ATLAS 2A CENTAUR R/B, 25674 (Decayed) |
EUTE 21A (EUTE W3) 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. |
|---|---|---|---|---|---|---|---|
| 26 mins | 2024-12-26 12:31:48.857Z | 108.443° ESE | 2024-12-26 12:31:48.857Z | 108.443° ESE | 10.56° | 2024-12-26 12:57:48.857Z | 109.375° ESE |
| 847 mins | 2024-12-26 22:24:48.857Z | 112.702° SE | 2024-12-27 06:30:48.857Z | 103.59° ESE | 20.42° | 2024-12-27 12:31:48.857Z | 112.654° SE |
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