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
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 OPS 8068
1 01580U 65072A 26285.32870107 .00000170 00000-0 63620-4 0 9994
2 01580 98.4363 78.1376 0229743 59.7697 302.6016 14.29719180149757Epoch: 2026-10-12T07:53Z
TLE epoch observation values (Epoch: 2026-10-12T07:53:19.772Z)
Latitude
-0.00001°
Longitude
-61.10348°
Altitude
709.562 km
Speed
7.546 km/s
True Right ascension
05h 12m 33s
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
23:02:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
954.478 km
Perigee altitude
625.122 km
Semi-major axis
7,167.937 km
Eccentricity
0.02297
Inclination
98.4363°
RAAN
78.1376°
Arg. of periapsis
59.7697°
True anomaly
300.3495°
Mean anomaly
302.6016°
Eccentric anomaly
301.47899°
Mean motion
3.57645 °/min
Orbital period
100.66 mins
BSTAR
0.00006362
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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 | 2026-10-13 09:14:14.516Z | 106.229° ESE | 2026-10-13 09:17:14.516Z | 59.235° ENE | 18.657° | 2026-10-13 09:19:14.516Z | 28.422° NE |
| 7 mins | 2026-10-13 10:53:14.516Z | 201.627° SSW | 2026-10-13 10:56:14.516Z | 261.654° W | 35.844° | 2026-10-13 11:00:14.516Z | 328.85° NNW |
| 9 mins | 2026-10-13 23:05:14.516Z | 18.626° NNE | 2026-10-13 23:09:14.516Z | 130.963° SE | 73.416° | 2026-10-13 23:14:14.516Z | 188.6° SSW |
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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