AURORA 1, 2876
Orbit data source: Space-Track
AURORA 1, 2876 is an American payload satellite in LEO that was launched on Thu, 29 Jun 1967 UTC via a THOR BURNER 2 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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2876 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Rice
Mission
Spacecraft
Bus & Motor
RICE AURORA, Unknown motor
Mass
21 kg wet, 21 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: 14 hours ago
TLE from 14 hours ago
0 AURORA 1
1 02876U 67065B 25339.91636885 -.00000028 00000-0 -18248-1 0 9991
2 02876 89.9883 313.4148 0070482 289.1463 70.1753 8.36560400373444Epoch: 2025-12-05T21:59Z
TLE epoch observation values (Epoch: 2025-12-05T21:59:34.268Z)
Latitude
-0.0001°
Longitude
-91.42958°
Altitude
3,850.268 km
Speed
6.251 km/s
True Right ascension
20h 53m 39s
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
09:53:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,942.262 km
Perigee altitude
3,797.799 km
Semi-major axis
10,248.168 km
Eccentricity
0.00705
Inclination
89.9883°
RAAN
313.4148°
Arg. of periapsis
289.1463°
True anomaly
70.93735°
Mean anomaly
70.1753°
Eccentric anomaly
70.5561°
Mean motion
2.09206 °/min
Orbital period
172.08 mins
BSTAR
-0.018248
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Other satellites on launch #65 in the year 1967 (1967-06-29 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.AURORA 1 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. |
|---|---|---|---|---|---|---|---|
| 29 mins | 2025-12-06 13:09:16.765Z | 350.216° N | 2025-12-06 13:23:16.765Z | 303.03° NW | 25.878° | 2025-12-06 13:38:16.765Z | 251.705° W |
| 35 mins | 2025-12-06 21:01:16.765Z | 134.429° SE | 2025-12-06 21:18:16.765Z | 67.74° E | 36.497° | 2025-12-06 21:36:16.765Z | 3.952° NNE |
| 37 mins | 2025-12-06 23:51:16.765Z | 205.193° SW | 2025-12-07 00:08:16.765Z | 276.007° WNW | 38.681° | 2025-12-07 00:28:16.765Z | 354.629° N |
| 38 mins | 2025-12-07 09:14:16.765Z | 6.579° NNE | 2025-12-07 09:33:16.765Z | 83.318° E | 39.207° | 2025-12-07 09:52:16.765Z | 158.426° S |
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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