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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 NIMBUS 2 DEB
1 26962U 66040M   26079.22256530  .00004003  00000-0  58405-2 0  9991
2 26962 100.3028 346.7855 0061220  15.3103 138.3730 13.54687473215587

Epoch: 2026-03-20T05:20Z

TLE epoch observation values (Epoch: 2026-03-20T05:20:29.641Z)

Latitude

25.43763°

Longitude

-86.16407°

Altitude

1,092.159 km

Speed

7.292 km/s

True Right ascension

11h 26m 52s

True Declination

25° 18' 38"

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

22:30:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,097.879 km

Perigee altitude

1,006.899 km

Semi-major axis

7,430.526 km

Eccentricity

0.00612

Inclination

100.3028°

RAAN

346.7855°

Arg. of periapsis

15.3103°

True anomaly

138.83635°

Mean anomaly

138.373°

Eccentric anomaly

138.60494°

Mean motion

3.38855 °/min

Orbital period

106.24 mins

BSTAR

0.0058405

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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.
9 mins	2026-03-20 18:52:22.114Z	215.074° SW	2026-03-20 18:57:22.114Z	269.742° W	21.474°	2026-03-20 19:01:22.114Z	312.869° NW
10 mins	2026-03-21 06:01:22.114Z	39.517° NE	2026-03-21 06:05:22.114Z	94.632° ESE	33.405°	2026-03-21 06:11:22.114Z	167.137° S
9 mins	2026-03-21 07:46:22.114Z	346.739° N	2026-03-21 07:50:22.114Z	291.659° WNW	29.574°	2026-03-21 07:55:22.114Z	236.556° WSW
7 mins	2026-03-21 16:13:22.114Z	89.745° E	2026-03-21 16:16:22.114Z	53.797° ENE	19.581°	2026-03-21 16:20:22.114Z	13.703° 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, 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: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-03-20T05:20:29.641Z)

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: 12 hours ago