NIMBUS 2 DEB, 39295

Orbit data source: Space-Track

NIMBUS 2 DEB, 39295 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/39295?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39295, 1966-040BD

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)

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

TLE from 2 days ago

0 NIMBUS 2 DEB
1 39295U 66040BD  26261.54888931  .00001508  00000-0  24308-2 0  9990
2 39295 100.4226 202.2141 0065986 317.9597  41.6482 13.49577538632909

Epoch: 2026-09-18T13:10Z

TLE epoch observation values (Epoch: 2026-09-18T13:10:24.036Z)

Latitude

-0°

Longitude

7.14376°

Altitude

1,039.967 km

Speed

7.35 km/s

True Right ascension

13h 28m 51s

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

18:20:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,120.308 km

Perigee altitude

1,021.999 km

Semi-major axis

7,449.29 km

Eccentricity

0.0066

Inclination

100.4226°

RAAN

202.2141°

Arg. of periapsis

317.9597°

True anomaly

42.15381°

Mean anomaly

41.6482°

Eccentric anomaly

41.90069°

Mean motion

3.37575 °/min

Orbital period

106.64 mins

BSTAR

0.0024308

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Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

THOR AGENA B R/B, 2174

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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	2026-09-20 08:28:16.374Z	28.686° NE	2026-09-20 08:34:16.374Z	94.989° ESE	46.469°	2026-09-20 08:40:16.374Z	170.536° S
9 mins	2026-09-20 10:15:16.374Z	347.048° N	2026-09-20 10:19:16.374Z	297.808° NW	32.728°	2026-09-20 10:24:16.374Z	241.659° WSW
8 mins	2026-09-20 18:43:16.374Z	100.387° ESE	2026-09-20 18:46:16.374Z	65.981° ENE	25.19°	2026-09-20 18:51:16.374Z	11.643° NNE
11 mins	2026-09-20 20:26:16.374Z	182.434° SSW	2026-09-20 20:31:16.374Z	256.35° W	58.2°	2026-09-20 20:37:16.374Z	335.217° NNW

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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, 39295 on other resources

View NIMBUS 2 DEB, 39295 on Heavens-Above

View NIMBUS 2 DEB, 39295 on Keep Track

View NIMBUS 2 DEB, 39295 on Celestrak

View NIMBUS 2 DEB, 39295 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, 39295

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: 2026-09-18T13:10:24.036Z)

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, 39295 on other resources

Documentation

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