OSCAR 3, 1293
Orbit data source: Space-Track
OSCAR 3, 1293 is a payload satellite owned by OSCAR (US) in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D 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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1293 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OSCAR
Mission
Non-operational spacecraft
Bus & Motor
OSCAR, Unknown motor
Mass
15 kg wet, 15 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: 7 hours ago
TLE from 7 hours ago
0 OSCAR 3
1 01293U 65016F 26038.26665134 .00000450 00000-0 29385-3 0 9994
2 01293 70.0757 321.7798 0019270 314.1465 45.8063 14.08370773113790Epoch: 2026-02-07T06:23Z
TLE epoch observation values (Epoch: 2026-02-07T06:23:58.675Z)
Latitude
0.00002°
Longitude
88.39269°
Altitude
857.566 km
Speed
7.429 km/s
True Right ascension
21h 27m 07s
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
15:35:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
876.93 km
Perigee altitude
849.022 km
Semi-major axis
7,241.113 km
Eccentricity
0.00193
Inclination
70.0757°
RAAN
321.7798°
Arg. of periapsis
314.1465°
True anomaly
45.96489°
Mean anomaly
45.8063°
Eccentric anomaly
45.88557°
Mean motion
3.52237 °/min
Orbital period
102.2 mins
BSTAR
0.00029385
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Other satellites on launch #16 in the year 1965 (1965-03-09 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.OSCAR 3 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 | 2026-02-07 20:09:24.738Z | 197.564° SSW | 2026-02-07 20:14:24.738Z | 79.663° E | 44.38° | 2026-02-07 20:19:24.738Z | 26.989° NE |
| 5 mins | 2026-02-07 21:57:24.738Z | 285.83° WNW | 2026-02-07 21:59:24.738Z | 309.795° NW | 16.44° | 2026-02-07 22:02:24.738Z | 344.517° N |
| 9 mins | 2026-02-08 05:07:24.738Z | 356.55° N | 2026-02-08 05:11:24.738Z | 60.85° ENE | 33.488° | 2026-02-08 05:16:24.738Z | 127.427° SE |
| 8 mins | 2026-02-08 06:52:24.738Z | 303.204° NW | 2026-02-08 06:55:24.738Z | 263.09° W | 25.402° | 2026-02-08 07:00:24.738Z | 200.321° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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