NIMBUS 2 DEB, 26962

Orbit data source: Space-Track

NIMBUS 2 DEB, 26962 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/26962?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26962, 1966-040M

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

Medium (>0.1 m² and <1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NIMBUS 2 DEB
1 26962U 66040M   26258.56495845  .00002113  00000-0  30838-2 0  9991
2 26962 100.2987 173.7488 0060903 312.1751 224.3583 13.55376537239871

Epoch: 2026-09-15T13:33Z

TLE epoch observation values (Epoch: 2026-09-15T13:33:32.410Z)

Latitude

3.79931°

Longitude

156.52253°

Altitude

1,087.398 km

Speed

7.293 km/s

True Right ascension

23h 37m 44s

True Declination

3° 46' 40"

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

06:47:48

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,095.107 km

Perigee altitude

1,004.63 km

Semi-major axis

7,428.005 km

Eccentricity

0.00609

Inclination

100.2987°

RAAN

173.7488°

Arg. of periapsis

312.1751°

True anomaly

223.87302°

Mean anomaly

224.3583°

Eccentric anomaly

224.11539°

Mean motion

3.39027 °/min

Orbital period

106.19 mins

BSTAR

0.0030838

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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	2026-09-16 17:10:08.090Z	118.733° SE	2026-09-16 17:15:08.090Z	66.428° ENE	29.465°	2026-09-16 17:20:08.090Z	8.896° NNE
10 mins	2026-09-16 18:55:08.090Z	191.742° SSW	2026-09-16 19:00:08.090Z	269.938° W	47.468°	2026-09-16 19:05:08.090Z	330.012° NNW
8 mins	2026-09-17 06:05:08.090Z	58.998° ENE	2026-09-17 06:08:08.090Z	91.637° ESE	21.381°	2026-09-17 06:13:08.090Z	140.806° SSE
11 mins	2026-09-17 07:48:08.090Z	7.116° NNE	2026-09-17 07:53:08.090Z	300.986° NW	64.689°	2026-09-17 07:59:08.090Z	211.405° 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, 26962 on other resources

View NIMBUS 2 DEB, 26962 on Heavens-Above

View NIMBUS 2 DEB, 26962 on Keep Track

View NIMBUS 2 DEB, 26962 on Celestrak

View NIMBUS 2 DEB, 26962 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, 26962

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-09-15T13:33:32.410Z)

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, 26962 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago