THOR BURNER 2 R/B, 3522

Orbit data source: Space-Track

THOR BURNER 2 R/B, 3522 is space debris in SSO originally from a launch on Wed, 23 Oct 1968 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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Iframe URL

https://www.satcat.com/sats-embedded/3522?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

3522, 1968-092B

Orbit

SSO

Country

Related business

USAF Space and Missile Systems Organization (US)

Manufacturer

Thiokol/TE

Mission

Spacecraft

Bus & Motor

STAR 37, Unknown motor

Mass

154 kg wet, 154 kg dry

Launch date (UTC)

1968-10-23 (58 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: 1 day ago

TLE from 1 day ago

0 THOR BURNER 2 R/B
1 03522U 68092B   26173.70513015  .00000122  00000-0  63502-4 0  9993
2 03522  98.8179 325.5855 0029454 149.5556 210.7344 14.31038673  1073

Epoch: 2026-06-22T16:55Z

TLE epoch observation values (Epoch: 2026-06-22T16:55:23.244Z)

Latitude

-0.00005°

Longitude

160.85144°

Altitude

809.35 km

Speed

7.439 km/s

True Right ascension

21h 42m 20s

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

14:46:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

806.51 km

Perigee altitude

764.311 km

Semi-major axis

7,163.547 km

Eccentricity

0.00295

Inclination

98.8179°

RAAN

325.5855°

Arg. of periapsis

149.5556°

True anomaly

210.56245°

Mean anomaly

210.7344°

Eccentric anomaly

210.64837°

Mean motion

3.57974 °/min

Orbital period

100.57 mins

BSTAR

0.000063502

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Other satellites on launch #92 in the year 1968 (1968-10-23 UTC)

OPS 4078 (DMSP 4B F2), 3510

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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	2026-06-24 09:19:59.275Z	127.203° SE	2026-06-24 09:23:59.275Z	65.67° ENE	29.23°	2026-06-24 09:27:59.275Z	7.764° NNE
7 mins	2026-06-24 10:59:59.275Z	213.589° SW	2026-06-24 11:02:59.275Z	257.794° W	25.19°	2026-06-24 11:06:59.275Z	317.611° NNW
8 mins	2026-06-24 23:12:59.275Z	8.669° NNE	2026-06-24 23:15:59.275Z	303.447° NW	44.329°	2026-06-24 23:20:59.275Z	200.234° SSW

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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, 3522 on other resources

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View THOR BURNER 2 R/B, 3522 on Celestrak

View THOR BURNER 2 R/B, 3522 on Gunter's Space Page

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THOR BURNER 2 R/B, 3522

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-06-22T16:55:23.244Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #92 in the year 1968 (1968-10-23 UTC)

THOR BURNER 2 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out THOR BURNER 2 R/B, 3522 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago