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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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 OPS 8068
1 01580U 65072A 25350.35786639 .00000542 00000-0 17470-3 0 9999
2 01580 98.3935 147.9906 0228591 225.7175 132.5056 14.29495567106893Epoch: 2025-12-16T08:35Z
TLE epoch observation values (Epoch: 2025-12-16T08:35:19.656Z)
Latitude
-0.00001°
Longitude
-66.08453°
Altitude
909.133 km
Speed
7.339 km/s
True Right ascension
09h 51m 57s
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
23:20:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
954.416 km
Perigee altitude
626.677 km
Semi-major axis
7,168.683 km
Eccentricity
0.02286
Inclination
98.3935°
RAAN
147.9906°
Arg. of periapsis
225.7175°
True anomaly
134.39975°
Mean anomaly
132.5056°
Eccentric anomaly
133.45633°
Mean motion
3.57589 °/min
Orbital period
100.67 mins
BSTAR
0.0001747
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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 | 2025-12-17 09:54:59.272Z | 132.935° SE | 2025-12-17 09:59:59.272Z | 62.897° ENE | 33.048° | 2025-12-17 10:04:59.272Z | 2.879° NNE |
| 8 mins | 2025-12-17 11:35:59.272Z | 217.27° SW | 2025-12-17 11:38:59.272Z | 259.5° W | 27.373° | 2025-12-17 11:43:59.272Z | 322.833° NNW |
| 8 mins | 2025-12-17 23:49:59.272Z | 4.542° NNE | 2025-12-17 23:53:59.272Z | 261.787° W | 42.063° | 2025-12-17 23:57:59.272Z | 205.963° 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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