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: 9 hours ago
TLE from 9 hours ago
0 OPS 8068
1 01580U 65072A 26002.29690613 .00001240 00000-0 37895-3 0 9992
2 01580 98.3949 164.3363 0229388 175.5828 184.7454 14.29525802109317Epoch: 2026-01-02T07:07Z
TLE epoch observation values (Epoch: 2026-01-02T07:07:32.689Z)
Latitude
-0°
Longitude
-44.48905°
Altitude
960.255 km
Speed
7.287 km/s
True Right ascension
10h 57m 20s
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
16:05:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
954.884 km
Perigee altitude
626.006 km
Semi-major axis
7,168.582 km
Eccentricity
0.02294
Inclination
98.3949°
RAAN
164.3363°
Arg. of periapsis
175.5828°
True anomaly
184.53399°
Mean anomaly
184.7454°
Eccentric anomaly
184.6391°
Mean motion
3.57597 °/min
Orbital period
100.67 mins
BSTAR
0.00037895
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-01-02 22:50:58.954Z | 38.666° NE | 2026-01-02 22:53:58.954Z | 84.801° E | 25.894° | 2026-01-02 22:57:58.954Z | 155.716° SSE |
| 5 mins | 2026-01-03 00:31:58.954Z | 328.452° NNW | 2026-01-03 00:33:58.954Z | 291.851° WNW | 21.807° | 2026-01-03 00:36:58.954Z | 244.546° WSW |
| 9 mins | 2026-01-03 10:07:58.954Z | 141.803° SSE | 2026-01-03 10:11:58.954Z | 87.419° E | 37.537° | 2026-01-03 10:16:58.954Z | 0.319° NNE |
| 7 mins | 2026-01-03 11:48:58.954Z | 226.449° WSW | 2026-01-03 11:51:58.954Z | 263.956° W | 21.003° | 2026-01-03 11:55:58.954Z | 312.885° 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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