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: 9 hours ago

TLE from 9 hours ago

0 NIMBUS 2 DEB
1 31579U 66040AR  26032.43682639  .00002238  00000-0  35617-2 0  9994
2 31579 100.5049   5.9351 0042291 109.7344  18.0588 13.50234485918031

Epoch: 2026-02-01T10:29Z

TLE epoch observation values (Epoch: 2026-02-01T10:29:01.800Z)

Latitude

50.93928°

Longitude

-89.83014°

Altitude

1,049.496 km

Speed

7.347 km/s

True Right ascension

13h 16m 17s

True Declination

50° 46' 39"

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

20:49:47

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,100.234 km

Perigee altitude

1,037.246 km

Semi-major axis

7,446.877 km

Eccentricity

0.00423

Inclination

100.5049°

RAAN

5.9351°

Arg. of periapsis

109.7344°

True anomaly

18.20979°

Mean anomaly

18.0588°

Eccentric anomaly

18.13422°

Mean motion

3.3774 °/min

Orbital period

106.59 mins

BSTAR

0.0035617

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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.
10 mins	2026-02-01 20:40:16.157Z	112.21° ESE	2026-02-01 20:45:16.157Z	60.511° ENE	23.18°	2026-02-01 20:50:16.157Z	8.67° NNE
10 mins	2026-02-01 22:25:16.157Z	184.722° SSW	2026-02-01 22:30:16.157Z	272.343° WNW	39.579°	2026-02-01 22:35:16.157Z	333.224° NNW
6 mins	2026-02-02 09:38:16.157Z	69.814° E	2026-02-02 09:40:16.157Z	91.401° ESE	16.331°	2026-02-02 09:44:16.157Z	130.808° SE
11 mins	2026-02-02 11:21:16.157Z	10.075° NNE	2026-02-02 11:26:16.157Z	263.431° W	43.614°	2026-02-02 11:32:16.157Z	205.437° SW

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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: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-02-01T10:29:01.800Z)

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: 9 hours ago