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: 19 hours ago
TLE from 19 hours ago
0 OPS 8068
1 01580U 65072A 26195.39708235 .00000045 00000-0 28292-4 0 9990
2 01580 98.4228 350.9944 0228125 325.5017 33.1536 14.29673467136905Epoch: 2026-07-14T09:31Z
TLE epoch observation values (Epoch: 2026-07-14T09:31:47.915Z)
Latitude
0.00004°
Longitude
-84.22308°
Altitude
659.927 km
Speed
7.598 km/s
True Right ascension
23h 23m 58s
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
16:59:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
953.474 km
Perigee altitude
626.43 km
Semi-major axis
7,168.089 km
Eccentricity
0.02281
Inclination
98.4228°
RAAN
350.9944°
Arg. of periapsis
325.5017°
True anomaly
34.61799°
Mean anomaly
33.1536°
Eccentric anomaly
33.88227°
Mean motion
3.57633 °/min
Orbital period
100.66 mins
BSTAR
0.000028292
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-15 09:12:41.905Z | 97.019° ESE | 2026-07-15 09:14:41.905Z | 69.036° E | 18.384° | 2026-07-15 09:18:41.905Z | 18.315° NNE |
| 8 mins | 2026-07-15 10:50:41.905Z | 191.548° SSW | 2026-07-15 10:54:41.905Z | 280.216° WNW | 36.044° | 2026-07-15 10:58:41.905Z | 333.964° NNW |
| 10 mins | 2026-07-15 23:03:41.905Z | 20.236° NNE | 2026-07-15 23:08:41.905Z | 109.917° ESE | 42.979° | 2026-07-15 23:13:41.905Z | 183.574° SSW |
| 6 mins | 2026-07-16 00:44:41.905Z | 330.738° NNW | 2026-07-16 00:47:41.905Z | 295.256° NW | 18.722° | 2026-07-16 00:50:41.905Z | 261.572° 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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