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: 11 hours ago
TLE from 11 hours ago
0 OPS 8068
1 1580U 65072A 26098.95407110 .00000315 00000-0 10788-3 0 9992
2 1580 98.4107 257.6908 0227929 250.0769 107.5730 14.29609676123124Epoch: 2026-04-08T22:53Z
TLE epoch observation values (Epoch: 2026-04-08T22:53:51.743Z)
Latitude
0.00004°
Longitude
77.01617°
Altitude
848.684 km
Speed
7.401 km/s
True Right ascension
17h 10m 45s
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
15:59:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
953.552 km
Perigee altitude
626.779 km
Semi-major axis
7,168.302 km
Eccentricity
0.02279
Inclination
98.4107°
RAAN
257.6908°
Arg. of periapsis
250.0769°
True anomaly
110.04098°
Mean anomaly
107.573°
Eccentric anomaly
108.8092°
Mean motion
3.57617 °/min
Orbital period
100.67 mins
BSTAR
0.00010788
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-04-09 10:45:57.896Z | 178.312° S | 2026-04-09 10:50:57.896Z | 270.245° WNW | 42.393° | 2026-04-09 10:55:57.896Z | 339.744° N |
| 8 mins | 2026-04-09 23:01:57.896Z | 29.639° NE | 2026-04-09 23:05:57.896Z | 116.879° SE | 38.312° | 2026-04-09 23:09:57.896Z | 174.278° S |
| 6 mins | 2026-04-10 00:41:57.896Z | 331.952° NNW | 2026-04-10 00:44:57.896Z | 291.91° WNW | 19.599° | 2026-04-10 00:47:57.896Z | 254.94° 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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