NIMBUS 2 DEB, 32475

Orbit data source: Space-Track

NIMBUS 2 DEB, 32475 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/32475?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

32475, 1966-040AS

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: 2 days ago

TLE from 2 days ago

0 NIMBUS 2 DEB
1 32475U 66040AS  26031.28238642  .00003302  00000-0  45621-2 0  9992
2 32475 100.5365  50.4812 0056001  73.5964 303.6397 13.58386804909835

Epoch: 2026-01-31T06:46Z

TLE epoch observation values (Epoch: 2026-01-31T06:46:38.186Z)

Latitude

16.39529°

Longitude

175.19261°

Altitude

1,020.826 km

Speed

7.354 km/s

True Right ascension

03h 09m 26s

True Declination

16° 18' 21"

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

17:45:11

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,080.432 km

Perigee altitude

997.359 km

Semi-major axis

7,417.033 km

Eccentricity

0.0056

Inclination

100.5365°

RAAN

50.4812°

Arg. of periapsis

73.5964°

True anomaly

303.10337°

Mean anomaly

303.6397°

Eccentric anomaly

303.37174°

Mean motion

3.3978 °/min

Orbital period

105.95 mins

BSTAR

0.0045621

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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.
10 mins	2026-02-03 00:14:14.525Z	127.361° SE	2026-02-03 00:19:14.525Z	55.312° ENE	32.443°	2026-02-03 00:24:14.525Z	359.835° N
9 mins	2026-02-03 01:59:14.525Z	209.15° SW	2026-02-03 02:03:14.525Z	262.106° W	27.883°	2026-02-03 02:08:14.525Z	321.571° NNW
8 mins	2026-02-03 13:06:14.525Z	51.317° ENE	2026-02-03 13:10:14.525Z	102.857° ESE	24.549°	2026-02-03 13:14:14.525Z	147.686° SSE
10 mins	2026-02-03 14:50:14.525Z	357.404° N	2026-02-03 14:54:14.525Z	297.566° NW	36.543°	2026-02-03 15:00:14.525Z	221.59° SW

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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, 32475 on other resources

View NIMBUS 2 DEB, 32475 on Heavens-Above

View NIMBUS 2 DEB, 32475 on Keep Track

View NIMBUS 2 DEB, 32475 on Celestrak

View NIMBUS 2 DEB, 32475 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, 32475

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-01-31T06:46:38.186Z)

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, 32475 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago