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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ISO8601 Format

Identifier

2422, 1966-082B

Orbit

SSO

Country

Related business

United States Space Force (US)

Manufacturer

Thiokol/TE

Mission

Spacecraft

Bus & Motor

STAR 37, Unknown motor

Mass

136 kg wet, 136 kg dry

Launch date (UTC)

1966-09-16 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago

0 THOR BURNER 2 R/B
1 02422U 66082B   25357.03360299  .00000300  00000-0  89214-4 0  9997
2 02422  98.2178 151.7014 0110844  25.1311 335.5219 14.46580058 89801

Epoch: 2025-12-23T00:48Z

TLE epoch observation values (Epoch: 2025-12-23T00:48:23.298Z)

Latitude

-0°

Longitude

47.78117°

Altitude

668.168 km

Speed

7.561 km/s

True Right ascension

10h 06m 48s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

19:19:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

812.773 km

Perigee altitude

655.107 km

Semi-major axis

7,112.077 km

Eccentricity

0.01108

Inclination

98.2178°

RAAN

151.7014°

Arg. of periapsis

25.1311°

True anomaly

334.9889°

Mean anomaly

335.5219°

Eccentric anomaly

335.25607°

Mean motion

3.61867 °/min

Orbital period

99.48 mins

BSTAR

0.000089214

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Other satellites on launch #82 in the year 1966 (1966-09-16 UTC)

OPS 6026 (DMSP 4A F1), 2418

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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.
9 mins	2025-12-23 22:57:17.151Z	25.832° NE	2025-12-23 23:01:17.151Z	84.967° E	37.266°	2025-12-23 23:06:17.151Z	174.313° S
5 mins	2025-12-24 00:37:17.151Z	329.098° NNW	2025-12-24 00:39:17.151Z	301.646° NW	18.26°	2025-12-24 00:42:17.151Z	259.665° W
7 mins	2025-12-24 10:08:17.151Z	145.69° SSE	2025-12-24 10:11:17.151Z	91.165° ESE	38.358°	2025-12-24 10:15:17.151Z	359.173° N

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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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Check out THOR BURNER 2 R/B, 2422 on other resources

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View THOR BURNER 2 R/B, 2422 on Celestrak

View THOR BURNER 2 R/B, 2422 on Gunter's Space Page

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THOR BURNER 2 R/B, 2422

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2025-12-23T00:48:23.298Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #82 in the year 1966 (1966-09-16 UTC)

THOR BURNER 2 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out THOR BURNER 2 R/B, 2422 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago