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 (60 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)

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Last TLE update: 4 hours ago

TLE from 4 hours ago

0 THOR BURNER 2 R/B
1 02422U 66082B   26077.66170224  .00000494  00000-0  13829-3 0  9995
2 02422  98.2303 234.8616 0111239 123.0169 238.1771 14.46700287102186

Epoch: 2026-03-18T15:52Z

TLE epoch observation values (Epoch: 2026-03-18T15:52:51.073Z)

Latitude

-0.00004°

Longitude

-179.57346°

Altitude

781.783 km

Speed

7.441 km/s

True Right ascension

15h 39m 26s

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

00:51:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

812.656 km

Perigee altitude

654.436 km

Semi-major axis

7,111.683 km

Eccentricity

0.01112

Inclination

98.2303°

RAAN

234.8616°

Arg. of periapsis

123.0169°

True anomaly

237.10195°

Mean anomaly

238.1771°

Eccentric anomaly

237.63873°

Mean motion

3.61897 °/min

Orbital period

99.48 mins

BSTAR

0.00013829

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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.
8 mins	2026-03-18 23:05:15.872Z	19.427° NNE	2026-03-18 23:09:15.872Z	77.503° E	41.658°	2026-03-18 23:13:15.872Z	182.036° SSW
8 mins	2026-03-19 10:16:15.872Z	158.244° S	2026-03-19 10:19:15.872Z	123.044° SE	43.2°	2026-03-19 10:24:15.872Z	350.624° 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

View THOR BURNER 2 R/B, 2422 on Heavens-Above

View THOR BURNER 2 R/B, 2422 on Keep Track

View THOR BURNER 2 R/B, 2422 on Celestrak

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

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

THOR BURNER 2 R/B, 2422

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 4 hours ago

TLE from 4 hours ago

TLE epoch observation values (Epoch: 2026-03-18T15:52:51.073Z)

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: 4 hours ago