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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Iframe URL

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: 20 hours ago

TLE from 20 hours ago

0 NIMBUS 2 DEB
1 31579U 66040AR  26078.67992528  .00001593  00000-0  25459-2 0  9997
2 31579 100.5050  54.6749 0047316   3.6782 169.2866 13.50425149924276

Epoch: 2026-03-19T16:19Z

TLE epoch observation values (Epoch: 2026-03-19T16:19:05.544Z)

Latitude

6.74736°

Longitude

173.92657°

Altitude

1,107.473 km

Speed

7.282 km/s

True Right ascension

15h 43m 42s

True Declination

6° 42' 33"

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

17:21:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,103.271 km

Perigee altitude

1,032.806 km

Semi-major axis

7,446.175 km

Eccentricity

0.00473

Inclination

100.505°

RAAN

54.6749°

Arg. of periapsis

3.6782°

True anomaly

169.38681°

Mean anomaly

169.2866°

Eccentric anomaly

169.33676°

Mean motion

3.37787 °/min

Orbital period

106.58 mins

BSTAR

0.0025459

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

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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.
4 mins	2026-03-20 13:23:55.315Z	327.625° NNW	2026-03-20 13:25:55.315Z	309.324° NW	12.36°	2026-03-20 13:27:55.315Z	290.742° WNW
11 mins	2026-03-20 21:48:55.315Z	146.516° SSE	2026-03-20 21:53:55.315Z	65.776° ENE	41.875°	2026-03-20 21:59:55.315Z	350.989° N
7 mins	2026-03-20 23:35:55.315Z	229.375° WSW	2026-03-20 23:38:55.315Z	261.659° W	18.974°	2026-03-20 23:42:55.315Z	305.285° NW
11 mins	2026-03-21 10:44:55.315Z	31.598° NE	2026-03-21 10:49:55.315Z	99.874° ESE	37.234°	2026-03-21 10:55:55.315Z	173.967° S

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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: 20 hours ago

TLE from 20 hours ago

TLE epoch observation values (Epoch: 2026-03-19T16:19:05.544Z)

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: 20 hours ago