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: 15 hours ago

TLE from 15 hours ago

0 NIMBUS 2 DEB
1 59975U 66040CE  26258.88747273  .00001780  00000-0  30727-2 0  9997
2 59975 100.1512  59.7150 0040586 297.8207  61.8812 13.45338288342530

Epoch: 2026-09-15T21:17Z

TLE epoch observation values (Epoch: 2026-09-15T21:17:57.643Z)

Latitude

-0.00012°

Longitude

105.37787°

Altitude

1,078.032 km

Speed

7.32 km/s

True Right ascension

03h 58m 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

05:09:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,117.088 km

Perigee altitude

1,056.493 km

Semi-major axis

7,464.928 km

Eccentricity

0.00406

Inclination

100.1512°

RAAN

59.715°

Arg. of periapsis

297.8207°

True anomaly

62.29237°

Mean anomaly

61.8812°

Eccentric anomaly

62.08669°

Mean motion

3.36515 °/min

Orbital period

106.98 mins

BSTAR

0.0030727

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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	2026-09-16 22:54:03.655Z	35.693° NE	2026-09-16 22:59:03.655Z	89.734° E	36.074°	2026-09-16 23:05:03.655Z	160.608° S
11 mins	2026-09-17 00:40:03.655Z	355.236° N	2026-09-17 00:45:03.655Z	291.29° WNW	40.281°	2026-09-17 00:51:03.655Z	228.317° WSW
7 mins	2026-09-17 09:11:03.655Z	89.285° E	2026-09-17 09:14:03.655Z	56.572° ENE	20.743°	2026-09-17 09:18:03.655Z	17.029° NNE
12 mins	2026-09-17 10:53:03.655Z	171.776° S	2026-09-17 10:59:03.655Z	283.862° WNW	71.904°	2026-09-17 11:05:03.655Z	340.694° 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: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-09-15T21:17:57.643Z)

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: 15 hours ago