SECOR 3, 1208
Orbit data source: Space-Track
SECOR 3, 1208 is an American payload satellite in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D launch vehicle from the Air Force Western Test Range (AFWTR). 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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1208 intel report (Beta)
SECOR 3 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | ITT |
| Mission | Defense Geodetic |
| Bus & Motor | SECOR, Unknown motor |
| Mass | 18 kg wet, 18 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, 0.4 m |
| Radar Cross Section | 0.105 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 SECOR 3
1 01208U 65016E 25001.63963559 .00000224 00000-0 20130-3 0 9990
2 01208 70.0783 236.1429 0017513 60.9450 329.8516 13.95945048 44983Epoch: 2025-01-01T15:21Z
Definitive object data (Epoch: 2025-01-01T15:21:04.514Z)
| Latitude | 28.7369° |
| Longitude | -84.25452° |
| Altitude | 899.802 km |
| Speed | 7.411 km/s |
| True Right ascension | 16h 30m 10s |
| True Declination | 28° 35' 42" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 29.82544° |
| Longitude | 70.23072° |
| Altitude | 910.653 km |
| Speed | 7.4 km/s |
| Apparent Right ascension | 03h 14m 37s |
| Apparent Declination | -2° 23' 20" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 15:48:54 |
| Azimuth | 13.894° NNE |
| Elevation | -51.675° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 918.662 km |
| Perigee altitude | 893.149 km |
| Semi-major axis | 7,284.043 km |
| Eccentricity | 0.0017513 |
| Inclination | 70.0783° |
| RAAN | 236.1429° |
| Arg. of periapsis | 60.945° |
| True anomaly | 329.75062° |
| Mean anomaly | 329.8516° |
| Eccentric anomaly | 329.80113° |
| Mean motion | 3.49128 °/min |
| BSTAR | 0.0002013 |
| Orbital period | 103.11 mins |
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Other satellites on launch #16 in the year 1965 (1965-03-09 UTC)
| OPS 4988 (GREB 6), 1271 |
| GGSE 2, 1244 |
| GGSE 3, 1292 |
| SOLRAD 7B, 1291 |
| SECOR 3, 1208 |
| OSCAR 3, 1293 |
| SURCAL 2, 1310 (Decayed) |
| PORCUPINE 1, 1272 |
| THOR AGENA D R/B, 1245 |
| OPS 4988 DEB, 12099 |
| GGSE 3 DEB, 44043 |
SECOR 3 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-01-02 17:07:12.449Z | 213.733° SW | 2025-01-02 17:13:12.449Z | 326.156° NNW | 42.121° | 2025-01-02 17:18:12.449Z | 18.887° NNE |
| 10 mins | 2025-01-03 02:10:12.449Z | 342.654° N | 2025-01-03 02:15:12.449Z | 94.456° ESE | 42.493° | 2025-01-03 02:20:12.449Z | 146.906° SSE |
| 6 mins | 2025-01-03 03:57:12.449Z | 288.499° WNW | 2025-01-03 03:59:12.449Z | 266.487° W | 15.885° | 2025-01-03 04:03:12.449Z | 223.698° SW |
| 7 mins | 2025-01-03 15:29:12.449Z | 143.879° SSE | 2025-01-03 15:32:12.449Z | 106.87° ESE | 21.846° | 2025-01-03 15:36:12.449Z | 57.307° ENE |
Authenticating...
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