NIMBUS 2 DEB, 59975

Orbit data source: Space-Track

NIMBUS 2 DEB, 59975 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/59975?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59975, 1966-040CE

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: 18 hours ago

TLE from 18 hours ago

0 NIMBUS 2 DEB
1 59975U 66040CE  25357.17208704  .00002426  00000-0  42328-2 0  9997
2 59975 100.1275 150.9308 0045216 226.6839 133.0517 13.44137681306684

Epoch: 2025-12-23T04:07Z

TLE epoch observation values (Epoch: 2025-12-23T04:07:48.320Z)

Latitude

0.00001°

Longitude

-2.98019°

Altitude

1,119.817 km

Speed

7.281 km/s

True Right ascension

10h 03m 43s

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

21:05:37

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,125.011 km

Perigee altitude

1,057.464 km

Semi-major axis

7,469.374 km

Eccentricity

0.00452

Inclination

100.1275°

RAAN

150.9308°

Arg. of periapsis

226.6839°

True anomaly

133.42886°

Mean anomaly

133.0517°

Eccentric anomaly

133.24043°

Mean motion

3.36215 °/min

Orbital period

107.07 mins

BSTAR

0.0042328

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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	2025-12-23 22:36:19.996Z	32.685° NE	2025-12-23 22:42:19.996Z	106.225° ESE	32.4°	2025-12-23 22:47:19.996Z	163.488° S
9 mins	2025-12-24 00:23:19.996Z	349.09° N	2025-12-24 00:27:19.996Z	296.916° NW	30.403°	2025-12-24 00:32:19.996Z	236.89° WSW
8 mins	2025-12-24 08:53:19.996Z	98.093° ESE	2025-12-24 08:57:19.996Z	53.886° ENE	21.635°	2025-12-24 09:01:19.996Z	14.401° NNE
12 mins	2025-12-24 10:36:19.996Z	176.788° S	2025-12-24 10:42:19.996Z	280.743° WNW	42.057°	2025-12-24 10:48:19.996Z	338.69° N

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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, 59975 on other resources

View NIMBUS 2 DEB, 59975 on Heavens-Above

View NIMBUS 2 DEB, 59975 on Keep Track

View NIMBUS 2 DEB, 59975 on Celestrak

View NIMBUS 2 DEB, 59975 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, 59975

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2025-12-23T04:07:48.320Z)

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, 59975 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 18 hours ago