OPS 8068, 1580
Orbit data source: Space-Track
OPS 8068, 1580 is a payload satellite owned by USAF SSD (US) in SSO that was launched on Fri, 10 Sep 1965 UTC via a THOR BURNER 1 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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1580 intel report (Beta)
OPS 8068 details
Identifier | |
Orbit | SSO |
Last TLE update | 4 hours ago |
Origin | |
Manufacturer | RCA/East Windsor |
Mission | Defense Weather |
Bus & Motor | P35, Unknown motor |
Mass | 72 kg wet, 72 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 0.6 m |
Radar Cross Section | 0.377 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 4 hours ago
0 OPS 8068
1 1580U 65072A 24356.46000075 .00001190 00000-0 36800-3 0 9997
2 1580 98.3546 161.6459 0230236 209.6031 149.1955 14.28995363 76029
Epoch: 2024-12-21T11:02Z
Definitive object data (Epoch: 2024-12-21T11:02:24.064Z)
Latitude | -0.00003° |
Longitude | -94.46521° |
Altitude | 940.88 km |
Speed | 7.308 km/s |
True Right ascension | 10h 46m 35s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 23.32679° |
Longitude | 89.31016° |
Altitude | 695.391 km |
Speed | 7.564 km/s |
Apparent Right ascension | 00h 22m 16s |
Apparent Declination | -7° 00' 27" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 14:11:01 |
Azimuth | 43.8° NE |
Elevation | -49.062° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 957.306 km |
Perigee altitude | 627.131 km |
Semi-major axis | 7,170.355 km |
Eccentricity | 0.0230236 |
Inclination | 98.3546° |
RAAN | 161.6459° |
Arg. of periapsis | 209.6031° |
True anomaly | 150.51387° |
Mean anomaly | 149.1955° |
Eccentric anomaly | 149.85791° |
Mean motion | 3.57464 °/min |
BSTAR | 0.000368 |
Orbital period | 100.71 mins |
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Other satellites on launch #72 in the year 1965 (1965-09-10 UTC)
OPS 8068, 1580 |
THOR ALTAIR DEB (YO), 1581 (Decayed) |
THOR ALTAIR DEB (YO), 1582 (Decayed) |
THOR ALTAIR R/B, 1583 |
THOR ALTAIR DEB, 1931 |
THOR ALTAIR DEB, 1932 (Decayed) |
OPS 8068 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. |
---|---|---|---|---|---|---|---|
8 mins | 2024-12-21 23:24:47.256Z | 36.129° NE | 2024-12-21 23:28:47.256Z | 98.323° ESE | 27.864° | 2024-12-21 23:32:47.256Z | 158.593° S |
6 mins | 2024-12-22 01:05:47.256Z | 334.134° NNW | 2024-12-22 01:07:47.256Z | 301.71° NW | 23.889° | 2024-12-22 01:11:47.256Z | 240.329° WSW |
10 mins | 2024-12-22 10:41:47.256Z | 141.01° SSE | 2024-12-22 10:46:47.256Z | 55.034° ENE | 37.632° | 2024-12-22 10:51:47.256Z | 358.087° N |
8 mins | 2024-12-22 12:22:47.256Z | 225.371° WSW | 2024-12-22 12:25:47.256Z | 262.505° W | 22.396° | 2024-12-22 12:30:47.256Z | 319.274° NNW |
Authenticating...
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