SECOR 4 (EGRS 4), 1315
Orbit data source: Space-Track
SECOR 4 (EGRS 4), 1315 is an American payload satellite in LEO that was launched on Sat, 03 Apr 1965 UTC via an ATLAS SLV-3 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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1315 intel report (Beta)
SECOR 4 (EGRS 4) details
Identifier | |
Orbit | LEO |
Last TLE update | 12 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 12 hours ago
0 SECOR 4 (EGRS 4)
1 01315U 65027B 25013.94969737 .00000054 00000-0 16912-3 0 9996
2 01315 90.2393 3.9409 0032709 114.8930 273.3616 12.92651570819846
Epoch: 2025-01-13T22:47Z
Definitive object data (Epoch: 2025-01-13T22:47:33.852Z)
Latitude | 27.9177° |
Longitude | -91.73972° |
Altitude | 1,293.049 km |
Speed | 7.213 km/s |
True Right ascension | 00h 15m 15s |
True Declination | 27° 47' 08" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 57.8486° |
Longitude | 88.77582° |
Altitude | 1,276.004 km |
Speed | 7.235 km/s |
Apparent Right ascension | 19h 33m 48s |
Apparent Declination | 54° 47' 19" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 11:01:30 |
Azimuth | 27.967° NE |
Elevation | 14.567° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 1,313.228 km |
Perigee altitude | 1,263.077 km |
Semi-major axis | 7,666.289 km |
Eccentricity | 0.0032709 |
Inclination | 90.2393° |
RAAN | 3.9409° |
Arg. of periapsis | 114.893° |
True anomaly | 272.98734° |
Mean anomaly | 273.3616° |
Eccentric anomaly | 273.17448° |
Mean motion | 3.23344 °/min |
BSTAR | 0.00016912 |
Orbital period | 111.34 mins |
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Other satellites on launch #27 in the year 1965 (1965-04-03 UTC)
SECOR 4 (EGRS 4) 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 | 2025-01-14 10:25:24.913Z | 28.067° NE | 2025-01-14 10:30:24.913Z | 77.481° E | 27.249° | 2025-01-14 10:36:24.913Z | 138.218° SSE |
12 mins | 2025-01-14 12:16:24.913Z | 346.796° N | 2025-01-14 12:22:24.913Z | 272.261° WNW | 36.574° | 2025-01-14 12:28:24.913Z | 211.504° SW |
13 mins | 2025-01-14 22:54:24.913Z | 151.076° SSE | 2025-01-14 23:00:24.913Z | 83.614° E | 38.539° | 2025-01-14 23:07:24.913Z | 8.083° NNE |
10 mins | 2025-01-15 00:47:24.913Z | 231.701° WSW | 2025-01-15 00:52:24.913Z | 284.774° WNW | 25.55° | 2025-01-15 00:57:24.913Z | 331.411° NNW |
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