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.
Focus sentinelFocus sentinel
1208 intel report (Beta)
Loading greatness...
SECOR 3 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 2 days 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 2 days ago
0 SECOR 3
1 01208U 65016E 24295.26738779 .00000192 00000-0 17803-3 0 9994
2 01208 70.0817 30.2495 0019207 167.8599 222.8972 13.95907194 34886Epoch: 2024-10-21T06:25Z
Definitive object data (Epoch: 2024-10-21T06:25:02.305Z)
| Latitude | 28.65578° |
| Longitude | -84.8459° |
| Altitude | 921.217 km |
| Speed | 7.389 km/s |
| True Right ascension | 02h 46m 26s |
| True Declination | 28° 30' 52" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 56.84709° |
| Longitude | -65.93018° |
| Altitude | 920.056 km |
| Speed | 7.396 km/s |
| Apparent Right ascension | 02h 47m 46s |
| Apparent Declination | 13° 18' 41" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 13:47:27 |
| Azimuth | 342.007° N |
| Elevation | -34.955° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 920.028 km |
| Perigee | 892.047 km |
| Semi-major axis | 7,284.174 km |
| Eccentricity | 0.0019207 |
| Inclination | 70.0817° |
| RAAN | 30.2495° |
| Arg. of periapsis | 167.8599° |
| True anomaly | 222.74765° |
| Mean anomaly | 222.8972° |
| Eccentric anomaly | 222.8224° |
| Mean motion | 3.49118 °/min |
| BSTAR | 0.00017803 |
| Period | 103.12 mins |
No data available
No data available
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: 39.9160978°, -105.1181434
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-10-22 19:01:10.900Z | 289.852° WNW | 2024-10-22 19:04:10.900Z | 256.823° W | 15.012° | 2024-10-22 19:06:10.900Z | 234.922° WSW |
| 8 mins | 2024-10-23 06:33:10.900Z | 146.21° SSE | 2024-10-23 06:36:10.900Z | 109.534° ESE | 23.013° | 2024-10-23 06:41:10.900Z | 50.834° ENE |
| 10 mins | 2024-10-23 08:17:10.900Z | 229.406° WSW | 2024-10-23 08:22:10.900Z | 308.507° NW | 36.55° | 2024-10-23 08:27:10.900Z | 12.291° NNE |
| 6 mins | 2024-10-23 15:35:10.900Z | 20.582° NNE | 2024-10-23 15:37:10.900Z | 43.298° NE | 16.127° | 2024-10-23 15:41:10.900Z | 86.508° E |
| 10 mins | 2024-10-23 17:19:10.900Z | 333.875° NNW | 2024-10-23 17:24:10.900Z | 196.408° SSW | 44.613° | 2024-10-23 17:29:10.900Z | 160.256° S |