NIMBUS 2 DEB, 38182

Orbit data source: Space-Track

NIMBUS 2 DEB, 38182 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/38182?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38182, 1966-040BA

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 38182U 66040BA  26124.38172868  .00002863  00000-0  37894-2 0  9998
2 38182 100.4507 177.6022 0083728 113.4976 262.1260 13.60386873601297

Epoch: 2026-05-04T09:09Z

TLE epoch observation values (Epoch: 2026-05-04T09:09:41.357Z)

Latitude

14.39955°

Longitude

175.20778°

Altitude

1,045.354 km

Speed

7.326 km/s

True Right ascension

11h 39m 36s

True Declination

14° 19' 12"

Sunlit

Object was in full shadow 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

06:45:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,093.654 km

Perigee altitude

969.573 km

Semi-major axis

7,409.751 km

Eccentricity

0.00837

Inclination

100.4507°

RAAN

177.6022°

Arg. of periapsis

113.4976°

True anomaly

261.177°

Mean anomaly

262.126°

Eccentric anomaly

261.65136°

Mean motion

3.40281 °/min

Orbital period

105.79 mins

BSTAR

0.0037894

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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.
7 mins	2026-05-06 01:51:47.284Z	94.893° ESE	2026-05-06 01:54:47.284Z	63.777° ENE	17.739°	2026-05-06 01:58:47.284Z	20.405° NNE
11 mins	2026-05-06 03:33:47.284Z	171.423° S	2026-05-06 03:38:47.284Z	247.479° WSW	43.852°	2026-05-06 03:44:47.284Z	340.253° N
10 mins	2026-05-06 16:24:47.284Z	20.694° NNE	2026-05-06 16:28:47.284Z	71.376° E	44.045°	2026-05-06 16:34:47.284Z	191.526° SSW
5 mins	2026-05-06 18:10:47.284Z	324.527° NNW	2026-05-06 18:12:47.284Z	301.415° NW	16.53°	2026-05-06 18:15:47.284Z	269.344° W

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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, 38182 on other resources

View NIMBUS 2 DEB, 38182 on Heavens-Above

View NIMBUS 2 DEB, 38182 on Keep Track

View NIMBUS 2 DEB, 38182 on Celestrak

View NIMBUS 2 DEB, 38182 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, 38182

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: 2026-05-04T09:09:41.357Z)

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, 38182 on other resources

Documentation

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