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, 0.050 m

Radar Cross Section

Small (<0.1 m²)

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Last TLE update: 4 days ago

TLE from 4 days ago

0 NIMBUS 2 DEB
1 38182U 66040BA  26302.01727176  .00002591  00000-0  34179-2 0  9995
2 38182 100.4978   7.7784 0057311  33.4235  88.0812 13.61487178625458

Epoch: 2026-10-29T00:24Z

TLE epoch observation values (Epoch: 2026-10-29T00:24:52.280Z)

Latitude

56.44283°

Longitude

160.33829°

Altitude

1,038.426 km

Speed

7.339 km/s

True Right ascension

13h 35m 39s

True Declination

56° 17' 25"

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

23:52:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,070.064 km

Perigee altitude

985.178 km

Semi-major axis

7,405.758 km

Eccentricity

0.00573

Inclination

100.4978°

RAAN

7.7784°

Arg. of periapsis

33.4235°

True anomaly

88.73771°

Mean anomaly

88.0812°

Eccentric anomaly

88.40944°

Mean motion

3.40556 °/min

Orbital period

105.71 mins

BSTAR

0.0034179

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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	2026-11-02 04:27:03.206Z	165.537° S	2026-11-02 04:33:03.206Z	312.598° NW	78.121°	2026-11-02 04:38:03.206Z	342.417° N
11 mins	2026-11-02 17:18:03.206Z	24.492° NE	2026-11-02 17:23:03.206Z	130.41° SE	66.532°	2026-11-02 17:29:03.206Z	187.405° SSW
7 mins	2026-11-02 19:03:03.206Z	336.399° NNW	2026-11-02 19:06:03.206Z	302.805° NW	21.394°	2026-11-02 19:10:03.206Z	260.136° W
8 mins	2026-11-03 03:26:03.206Z	112.64° SE	2026-11-03 03:30:03.206Z	54.432° ENE	31.95°	2026-11-03 03:34:03.206Z	7.729° NNE

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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: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2026-10-29T00:24:52.280Z)

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: 4 days ago