SYNCOM 2 (A 26), 634
Orbit data source: Space-Track
SYNCOM 2 (A 26), 634 is a payload satellite owned by GSFC (US) in GEO that was launched on Fri, 26 Jul 1963 UTC via a THOR DELTA B 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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634 intel report (Beta)
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SYNCOM 2 (A 26) details
| Identifier | |
| Orbit | GEO |
| Last TLE update | 13 hours ago |
| Origin | |
| Manufacturer | Hughes |
| Mission | Non-operational Civil Communications |
| Bus & Motor | HS-301, JPL SR-12-1 |
| Mass | 66 kg wet, ~30 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 0.71 m |
| Radar Cross Section | 0.415 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 13 hours ago
0 SYNCOM 2 (A 26)
1 00634U 63031A 24302.57714348 -.00000061 00000-0 00000-0 0 9994
2 00634 31.2571 308.8370 0009519 202.6832 164.2901 1.00293517224380Epoch: 2024-10-28T13:51Z
Definitive object data (Epoch: 2024-10-28T13:51:05.196Z)
| Latitude | 3.63383° |
| Longitude | 69.65466° |
| Altitude | 35,818.422 km |
| Speed | 3.072 km/s |
| True Right ascension | 20h 59m 18s |
| True Declination | 3° 37' 49" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -13.21494° |
| Longitude | -93.60205° |
| Altitude | 35,743.044 km |
| Speed | 3.078 km/s |
| Apparent Right ascension | 10h 09m 30s |
| Apparent Declination | -16° 37' 09" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 22:36:31 |
| Azimuth | 16.069° NNE |
| Elevation | -65.975° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 35,821.284 km |
| Perigee | 35,741.021 km |
| Semi-major axis | 42,159.289 km |
| Eccentricity | 0.0009519 |
| Inclination | 31.2571° |
| RAAN | 308.837° |
| Arg. of periapsis | 202.6832° |
| True anomaly | 164.3196° |
| Mean anomaly | 164.2901° |
| Eccentric anomaly | 164.30485° |
| Mean motion | 0.25073 °/min |
| BSTAR | Unknown |
| Period | 1435.82 mins |
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Other satellites on launch #31 in the year 1963 (1963-07-26 UTC)
| SYNCOM 2 (A 26), 634 |
| DELTA 1 R/B, 625 (Decayed) |
SYNCOM 2 (A 26) 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. |
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