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: 6 hours ago
TLE from 6 hours ago
0 OPS 8068
1 01580U 65072A 26070.95836105 .00000216 00000-0 78716-4 0 9998
2 01580 98.4054 230.6298 0228512 333.1741 25.7770 14.29589164119129Epoch: 2026-03-11T23:00Z
TLE epoch observation values (Epoch: 2026-03-11T23:00:02.394Z)
Latitude
-0.00003°
Longitude
76.0047°
Altitude
649.18 km
Speed
7.61 km/s
True Right ascension
15h 22m 31s
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
09:10:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
954.039 km
Perigee altitude
626.428 km
Semi-major axis
7,168.371 km
Eccentricity
0.02285
Inclination
98.4054°
RAAN
230.6298°
Arg. of periapsis
333.1741°
True anomaly
26.94568°
Mean anomaly
25.777°
Eccentric anomaly
26.3583°
Mean motion
3.57612 °/min
Orbital period
100.67 mins
BSTAR
0.000078716
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-12 09:14:39.006Z | 95.808° ESE | 2026-03-12 09:17:39.006Z | 55.663° ENE | 15.624° | 2026-03-12 09:19:39.006Z | 30.288° NE |
| 7 mins | 2026-03-12 10:53:39.006Z | 190.352° SSW | 2026-03-12 10:56:39.006Z | 280.342° WNW | 39.229° | 2026-03-12 11:00:39.006Z | 336.99° NNW |
| 9 mins | 2026-03-12 23:06:39.006Z | 27.064° NE | 2026-03-12 23:10:39.006Z | 105.717° ESE | 40.875° | 2026-03-12 23:15:39.006Z | 178.27° S |
| 7 mins | 2026-03-13 00:46:39.006Z | 332.877° NNW | 2026-03-13 00:49:39.006Z | 295.534° NW | 20.847° | 2026-03-13 00:53:39.006Z | 251.093° W |
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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