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 | 6 hours 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 6 hours ago
0 SECOR 3
1 1208U 65016E 25018.47649491 .00000104 00000-0 11401-3 0 9994
2 1208 70.0774 200.2891 0018249 36.2367 344.6422 13.95951577 47807Epoch: 2025-01-18T11:26Z
Definitive object data (Epoch: 2025-01-18T11:26:09.16Z)
| Latitude | 19.53606° |
| Longitude | -82.02438° |
| Altitude | 896.897 km |
| Speed | 7.412 km/s |
| True Right ascension | 13h 50m 33s |
| True Declination | 19° 25' 48" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 25.17857° |
| Longitude | 80.3537° |
| Altitude | 916.367 km |
| Speed | 7.393 km/s |
| Apparent Right ascension | 02h 54m 06s |
| Apparent Declination | -6° 23' 45" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 18:06:32 |
| Azimuth | 65.292° ENE |
| Elevation | -35.482° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 919.176 km |
| Perigee altitude | 892.591 km |
| Semi-major axis | 7,284.02 km |
| Eccentricity | 0.0018249 |
| Inclination | 70.0774° |
| RAAN | 200.2891° |
| Arg. of periapsis | 36.2367° |
| True anomaly | 344.58669° |
| Mean anomaly | 344.6422° |
| Eccentric anomaly | 344.61446° |
| Mean motion | 3.49129 °/min |
| BSTAR | 0.00011401 |
| 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-01-18 22:12:33.256Z | 356.902° N | 2025-01-18 22:16:33.256Z | 47.615° ENE | 29.539° | 2025-01-18 22:21:33.256Z | 117.475° SE |
| 9 mins | 2025-01-18 23:58:33.256Z | 311.498° NW | 2025-01-19 00:02:33.256Z | 254.849° W | 30.43° | 2025-01-19 00:07:33.256Z | 192.069° SSW |
| 10 mins | 2025-01-19 13:15:33.256Z | 198.087° SSW | 2025-01-19 13:20:33.256Z | 56.3° ENE | 44.017° | 2025-01-19 13:25:33.256Z | 26.532° NE |
| 5 mins | 2025-01-19 15:04:33.256Z | 289.384° WNW | 2025-01-19 15:06:33.256Z | 313.352° NW | 16.565° | 2025-01-19 15:09:33.256Z | 346.63° N |
Authenticating...
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