NIMBUS 2 DEB, 59972

Orbit data source: Space-Track

NIMBUS 2 DEB, 59972 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/59972?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59972, 1966-040CB

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)

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Last TLE update: 4 hours ago

TLE from 4 hours ago

0 NIMBUS 2 DEB
1 59972U 66040CB  25344.51974654  .00002075  00000-0  39211-2 0  9999
2 59972 100.4547 183.3127 0049857 343.2561  16.6917 13.39175107234496

Epoch: 2025-12-10T12:28Z

TLE epoch observation values (Epoch: 2025-12-10T12:28:26.101Z)

Latitude

-0.00001°

Longitude

-83.28496°

Altitude

1,079.335 km

Speed

7.33 km/s

True Right ascension

12h 13m 15s

True Declination

0° 00' 00"

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

14:53:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,147.042 km

Perigee altitude

1,072.377 km

Semi-major axis

7,487.846 km

Eccentricity

0.00499

Inclination

100.4547°

RAAN

183.3127°

Arg. of periapsis

343.2561°

True anomaly

16.85678°

Mean anomaly

16.6917°

Eccentric anomaly

16.77414°

Mean motion

3.34971 °/min

Orbital period

107.47 mins

BSTAR

0.0039211

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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.
12 mins	2025-12-11 01:38:08.143Z	33.398° NE	2025-12-11 01:44:08.143Z	108.619° ESE	33.508°	2025-12-11 01:50:08.143Z	168.658° S
10 mins	2025-12-11 03:25:08.143Z	350.377° N	2025-12-11 03:29:08.143Z	301.625° NW	30.61°	2025-12-11 03:35:08.143Z	234.784° WSW
8 mins	2025-12-11 11:57:08.143Z	101.856° ESE	2025-12-11 12:01:08.143Z	55.827° ENE	22.932°	2025-12-11 12:05:08.143Z	13.758° NNE
11 mins	2025-12-11 13:41:08.143Z	181.582° SSW	2025-12-11 13:46:08.143Z	252.97° W	40.703°	2025-12-11 13:52:08.143Z	335.212° 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, 59972 on other resources

View NIMBUS 2 DEB, 59972 on Heavens-Above

View NIMBUS 2 DEB, 59972 on Keep Track

View NIMBUS 2 DEB, 59972 on Celestrak

View NIMBUS 2 DEB, 59972 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, 59972

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: 2025-12-10T12:28:26.101Z)

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, 59972 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 4 hours ago