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, 0.055 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 NIMBUS 2 DEB
1 59975U 66040CE  26305.88514385  .00001699  00000-0  29266-2 0  9991
2 59975 100.1537 107.2083 0042842 187.8783 172.1679 13.45510602348855

Epoch: 2026-11-01T21:14Z

TLE epoch observation values (Epoch: 2026-11-01T21:14:36.428Z)

Latitude

-0.00001°

Longitude

107.38642°

Altitude

1,123.285 km

Speed

7.276 km/s

True Right ascension

07h 08m 49s

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

06:42:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,118.131 km

Perigee altitude

1,054.174 km

Semi-major axis

7,464.29 km

Eccentricity

0.00428

Inclination

100.1537°

RAAN

107.2083°

Arg. of periapsis

187.8783°

True anomaly

172.23445°

Mean anomaly

172.1679°

Eccentric anomaly

172.20121°

Mean motion

3.36558 °/min

Orbital period

106.97 mins

BSTAR

0.0029266

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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	2026-11-02 11:36:37.717Z	195.678° SSW	2026-11-02 11:42:37.717Z	260.084° W	37.963°	2026-11-02 11:48:37.717Z	327.261° NNW
9 mins	2026-11-02 22:51:37.717Z	44.338° NE	2026-11-02 22:55:37.717Z	91.396° ESE	30.3°	2026-11-02 23:00:37.717Z	151.266° SSE
10 mins	2026-11-03 00:36:37.717Z	358.053° N	2026-11-03 00:41:37.717Z	289.61° WNW	44.693°	2026-11-03 00:46:37.717Z	227.011° WSW
7 mins	2026-11-03 09:07:37.717Z	87.384° E	2026-11-03 09:10:37.717Z	57.225° ENE	18.421°	2026-11-03 09:14:37.717Z	18.952° NNE
6 mins	2026-11-03 10:49:37.717Z	166.128° S	2026-11-03 10:55:37.717Z	307.618° NW	80.05°	2026-11-03 10:55:37.717Z	307.618° NW

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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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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: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-11-01T21:14:36.428Z)

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: 14 hours ago