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: 10 hours ago
TLE from 10 hours ago
0 OPS 8068
1 1580U 65072A 25321.44949084 .00000541 00000-0 17489-3 0 9991
2 1580 98.3925 120.0988 0228567 311.5514 46.6264 14.29455008102762Epoch: 2025-11-17T10:47Z
TLE epoch observation values (Epoch: 2025-11-17T10:47:16.008Z)
Latitude
-0.00008°
Longitude
-98.46765°
Altitude
685.925 km
Speed
7.571 km/s
True Right ascension
08h 00m 23s
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
17:43:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
954.537 km
Perigee altitude
626.826 km
Semi-major axis
7,168.819 km
Eccentricity
0.02286
Inclination
98.3925°
RAAN
120.0988°
Arg. of periapsis
311.5514°
True anomaly
48.56796°
Mean anomaly
46.6264°
Eccentric anomaly
47.59337°
Mean motion
3.57579 °/min
Orbital period
100.68 mins
BSTAR
0.00017489
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-17 23:07:35.498Z | 24.968° NE | 2025-11-17 23:12:35.498Z | 89.215° E | 38.214° | 2025-11-17 23:18:35.498Z | 175.166° S |
| 8 mins | 2025-11-18 00:48:35.498Z | 338.628° N | 2025-11-18 00:51:35.498Z | 302.15° NW | 23.083° | 2025-11-18 00:56:35.498Z | 244.117° WSW |
| 8 mins | 2025-11-18 10:26:35.498Z | 148.698° SSE | 2025-11-18 10:29:35.498Z | 82.793° E | 42.071° | 2025-11-18 10:34:35.498Z | 353.699° N |
| 4 mins | 2025-11-18 12:08:35.498Z | 254.877° W | 2025-11-18 12:09:35.498Z | 267.673° W | 13.907° | 2025-11-18 12:12:35.498Z | 302.817° NW |
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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