NIMBUS 2 DEB, 39294

Orbit data source: Space-Track

NIMBUS 2 DEB, 39294 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/39294?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39294, 1966-040BC

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, 0.086 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago

0 NIMBUS 2 DEB
1 39294U 66040BC  26308.03614828  .00001284  00000-0  21618-2 0  9999
2 39294 100.4422 218.1022 0044832 200.0749 159.8619 13.47591321638520

Epoch: 2026-11-04T00:52Z

TLE epoch observation values (Epoch: 2026-11-04T00:52:03.211Z)

Latitude

-0.00001°

Longitude

161.79859°

Altitude

1,115.31 km

Speed

7.28 km/s

True Right ascension

14h 32m 24s

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

10:03:48

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,111.907 km

Perigee altitude

1,045.048 km

Semi-major axis

7,456.615 km

Eccentricity

0.00448

Inclination

100.4422°

RAAN

218.1022°

Arg. of periapsis

200.0749°

True anomaly

160.03785°

Mean anomaly

159.8619°

Eccentric anomaly

159.94996°

Mean motion

3.37078 °/min

Orbital period

106.8 mins

BSTAR

0.0021618

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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	2026-11-04 17:01:55.957Z	125.796° SE	2026-11-04 17:07:55.957Z	57.449° ENE	36.138°	2026-11-04 17:12:55.957Z	3.504° NNE
11 mins	2026-11-04 18:47:55.957Z	198.935° SSW	2026-11-04 18:52:55.957Z	266.181° W	40.643°	2026-11-04 18:58:55.957Z	329.433° NNW
9 mins	2026-11-05 06:00:55.957Z	48.896° ENE	2026-11-05 06:04:55.957Z	95.741° ESE	26.679°	2026-11-05 06:09:55.957Z	149.465° SSE
10 mins	2026-11-05 07:45:55.957Z	359.334° N	2026-11-05 07:49:55.957Z	306.18° NW	49.782°	2026-11-05 07:55:55.957Z	221.201° 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, 39294 on other resources

View NIMBUS 2 DEB, 39294 on Heavens-Above

View NIMBUS 2 DEB, 39294 on Keep Track

View NIMBUS 2 DEB, 39294 on Celestrak

View NIMBUS 2 DEB, 39294 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, 39294

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-11-04T00:52:03.211Z)

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, 39294 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 13 hours ago