NIMBUS 2 DEB, 31579

Orbit data source: Space-Track

NIMBUS 2 DEB, 31579 is space debris in SSO originally from a launch on Sun, 15 May 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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https://www.satcat.com/sats-embedded/31579?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

31579, 1966-040AR

Orbit

SSO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-05-15 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago

0 NIMBUS 2 DEB
1 31579U 66040AR  26133.49080477  .00001095  00000-0  17734-2 0  9994
2 31579 100.5025 112.4639 0040280 228.8052 258.0488 13.50622217931677

Epoch: 2026-05-13T11:46Z

TLE epoch observation values (Epoch: 2026-05-13T11:46:45.532Z)

Latitude

52.41309°

Longitude

-101.6127°

Altitude

1,084.687 km

Speed

7.312 km/s

True Right ascension

20h 25m 18s

True Declination

52° 15' 14"

Sunlit

Object was in daylight 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

16:51:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,097.304 km

Perigee altitude

1,037.323 km

Semi-major axis

7,445.45 km

Eccentricity

0.00403

Inclination

100.5025°

RAAN

112.4639°

Arg. of periapsis

228.8052°

True anomaly

257.59771°

Mean anomaly

258.0488°

Eccentric anomaly

257.8232°

Mean motion

3.37837 °/min

Orbital period

106.56 mins

BSTAR

0.0017734

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Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

THOR AGENA B R/B, 2174

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NIMBUS 2 DEB 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.
11 mins	2026-05-14 10:52:26.666Z	32.313° NE	2026-05-14 10:57:26.666Z	90.086° ESE	34.109°	2026-05-14 11:03:26.666Z	168.466° S
9 mins	2026-05-14 12:38:26.666Z	349.496° N	2026-05-14 12:42:26.666Z	300.735° NW	28.439°	2026-05-14 12:47:26.666Z	240.757° WSW
8 mins	2026-05-14 21:06:26.666Z	98.536° ESE	2026-05-14 21:09:26.666Z	64.597° ENE	22.759°	2026-05-14 21:14:26.666Z	11.594° NNE
11 mins	2026-05-14 22:49:26.666Z	181.288° SSW	2026-05-14 22:54:26.666Z	263.979° W	41.176°	2026-05-14 23:00:26.666Z	336.264° NNW

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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 NIMBUS 2 DEB, 31579 on other resources

View NIMBUS 2 DEB, 31579 on Heavens-Above

View NIMBUS 2 DEB, 31579 on Keep Track

View NIMBUS 2 DEB, 31579 on Celestrak

View NIMBUS 2 DEB, 31579 on Gunter's Space Page

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

NIMBUS 2 DEB, 31579

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 21 hours ago

TLE from 21 hours ago

TLE epoch observation values (Epoch: 2026-05-13T11:46:45.532Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

NIMBUS 2 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out NIMBUS 2 DEB, 31579 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 21 hours ago