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

Medium (>0.1 m² and <1 m²)

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

TLE from 1 day ago

0 NIMBUS 2 DEB
1 59972U 66040CB  26215.01702205  .00000993  00000-0  19066-2 0  9996
2 59972 100.4414  65.7158 0043519 144.3576 216.0469 13.39824324266025

Epoch: 2026-08-03T00:24Z

TLE epoch observation values (Epoch: 2026-08-03T00:24:30.705Z)

Latitude

-0.00002°

Longitude

107.98169°

Altitude

1,139.081 km

Speed

7.271 km/s

True Right ascension

04h 22m 51s

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

16:53:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,139.864 km

Perigee altitude

1,074.712 km

Semi-major axis

7,485.425 km

Eccentricity

0.00435

Inclination

100.4414°

RAAN

65.7158°

Arg. of periapsis

144.3576°

True anomaly

215.75473°

Mean anomaly

216.0469°

Eccentric anomaly

215.90069°

Mean motion

3.35134 °/min

Orbital period

107.42 mins

BSTAR

0.0019066

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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.
11 mins	2026-08-04 03:52:32.789Z	0.24° NNE	2026-08-04 03:57:32.789Z	305.638° NW	33.828°	2026-08-04 04:03:32.789Z	227.833° WSW
7 mins	2026-08-04 12:26:32.789Z	89.372° E	2026-08-04 12:29:32.789Z	56.945° ENE	19.548°	2026-08-04 12:33:32.789Z	17.02° NNE
11 mins	2026-08-04 14:09:32.789Z	172.225° S	2026-08-04 14:14:32.789Z	249.062° W	43.881°	2026-08-04 14:20:32.789Z	339.726° N
6 mins	2026-08-05 01:27:32.789Z	65.217° ENE	2026-08-05 01:30:32.789Z	94.449° ESE	14.097°	2026-08-05 01:33:32.789Z	122.278° SE

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-08-03T00:24:30.705Z)

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: 1 day ago