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: 14 hours ago
TLE from 14 hours ago
0 OPS 8068
1 01580U 65072A 26145.49733549 .00000336 00000-0 11217-3 0 9993
2 01580 98.4174 302.7058 0230090 112.5819 249.9884 14.29646654129772Epoch: 2026-05-25T11:56Z
TLE epoch observation values (Epoch: 2026-05-25T11:56:09.786Z)
Latitude
-0.00004°
Longitude
-119.41925°
Altitude
855.641 km
Speed
7.394 km/s
True Right ascension
20h 10m 49s
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
11:17:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
954.974 km
Perigee altitude
625.109 km
Semi-major axis
7,168.179 km
Eccentricity
0.02301
Inclination
98.4174°
RAAN
302.7058°
Arg. of periapsis
112.5819°
True anomaly
247.53586°
Mean anomaly
249.9884°
Eccentric anomaly
248.75964°
Mean motion
3.57627 °/min
Orbital period
100.66 mins
BSTAR
0.00011217
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-26 09:53:48.865Z | 139.737° SSE | 2026-05-26 09:57:48.865Z | 80.853° E | 33.901° | 2026-05-26 10:01:48.865Z | 4.767° NNE |
| 5 mins | 2026-05-26 11:35:48.865Z | 235.975° WSW | 2026-05-26 11:37:48.865Z | 265.891° W | 18.424° | 2026-05-26 11:40:48.865Z | 307.681° NW |
| 6 mins | 2026-05-26 23:47:48.865Z | 352.131° N | 2026-05-26 23:49:48.865Z | 307.763° NW | 36.642° | 2026-05-26 23:53:48.865Z | 215.509° 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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