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). Payload-class satellites include a variety of spacecraft 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)
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Identifier
Orbit
Country
USRelated business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
P35, Unknown motor
Mass
72 kg wet, 72 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OPS 8068
1 01580U 65072A 26134.99901190 .00000246 00000-0 86120-4 0 9991
2 01580 98.4161 292.5505 0229779 143.4548 218.2565 14.29639773128278Epoch: 2026-05-14T23:58Z
TLE epoch observation values (Epoch: 2026-05-14T23:58:34.628Z)
Latitude
0.00005°
Longitude
60.16958°
Altitude
926.705 km
Speed
7.321 km/s
True Right ascension
19h 30m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:44:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
954.775 km
Perigee altitude
625.355 km
Semi-major axis
7,168.202 km
Eccentricity
0.02298
Inclination
98.4161°
RAAN
292.5505°
Arg. of periapsis
143.4548°
True anomaly
216.66234°
Mean anomaly
218.2565°
Eccentric anomaly
217.45585°
Mean motion
3.57625 °/min
Orbital period
100.66 mins
BSTAR
0.00008612
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Other satellites on launch #72 in the year 1965 (1965-09-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OPS 8068 Visibility forecast
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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 | 2026-05-16 09:41:55.453Z | 132.154° SE | 2026-05-16 09:46:55.453Z | 58.989° ENE | 29.605° | 2026-05-16 09:50:55.453Z | 6.269° NNE |
| 7 mins | 2026-05-16 11:22:55.453Z | 216.636° SW | 2026-05-16 11:25:55.453Z | 261.531° W | 25.307° | 2026-05-16 11:29:55.453Z | 318.701° NNW |
| 7 mins | 2026-05-16 23:35:55.453Z | 4.891° NNE | 2026-05-16 23:38:55.453Z | 284.137° WNW | 42.845° | 2026-05-16 23:42:55.453Z | 203.707° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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