THOR BURNER 2 R/B, 2422
Orbit data source: Space-Track
THOR BURNER 2 R/B, 2422 is space debris in SSO originally from a launch on Fri, 16 Sep 1966 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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2422 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 37, Unknown motor
Mass
136 kg wet, 136 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Sphere + Cone + 1 Truss, 0.8 m
Radar Cross Section
2.270 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 THOR BURNER 2 R/B
1 02422U 66082B 25259.01553219 .00000278 00000-0 84248-4 0 9998
2 02422 98.2104 56.6292 0109888 324.1090 35.2755 14.46413423 75639Epoch: 2025-09-16T00:22Z
TLE epoch observation values (Epoch: 2025-09-16T00:22:21.981Z)
Latitude
0.00003°
Longitude
55.82571°
Altitude
676.797 km
Speed
7.552 km/s
True Right ascension
03h 46m 31s
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
06:57:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
812.645 km
Perigee altitude
656.327 km
Semi-major axis
7,112.623 km
Eccentricity
0.01099
Inclination
98.2104°
RAAN
56.6292°
Arg. of periapsis
324.109°
True anomaly
36.01094°
Mean anomaly
35.2755°
Eccentric anomaly
35.64239°
Mean motion
3.61825 °/min
Orbital period
99.5 mins
BSTAR
0.000084248
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Other satellites on launch #82 in the year 1966 (1966-09-16 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.THOR BURNER 2 R/B 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 | 2025-09-16 22:33:12.704Z | 45.414° ENE | 2025-09-16 22:36:12.704Z | 86.599° E | 24.043° | 2025-09-16 22:40:12.704Z | 145.241° SSE |
| 7 mins | 2025-09-17 00:12:12.704Z | 343.821° N | 2025-09-17 00:15:12.704Z | 287.53° WNW | 31.564° | 2025-09-17 00:19:12.704Z | 227.974° WSW |
| 6 mins | 2025-09-17 09:44:12.704Z | 109.409° ESE | 2025-09-17 09:46:12.704Z | 74.538° E | 24.907° | 2025-09-17 09:50:12.704Z | 13.132° NNE |
| 6 mins | 2025-09-17 11:22:12.704Z | 215.293° SW | 2025-09-17 11:25:12.704Z | 271.964° WNW | 26.579° | 2025-09-17 11:28:12.704Z | 318.713° NNW |
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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