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: 11 hours ago

TLE from 11 hours ago

0 NIMBUS 2 DEB
1 26962U 66040M   25336.22113686  .00002444  00000-0  36311-2 0  9999
2 26962 100.2989 234.3483 0055861 282.4690 230.0122 13.54165736200967

Epoch: 2025-12-02T05:18Z

TLE epoch observation values (Epoch: 2025-12-02T05:18:26.224Z)

Latitude

27.55774°

Longitude

-91.15706°

Altitude

1,087.05 km

Speed

7.298 km/s

True Right ascension

03h 59m 02s

True Declination

27° 25' 23"

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

13:47:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,095.817 km

Perigee altitude

1,012.78 km

Semi-major axis

7,432.436 km

Eccentricity

0.00559

Inclination

100.2989°

RAAN

234.3483°

Arg. of periapsis

282.469°

True anomaly

229.52395°

Mean anomaly

230.0122°

Eccentric anomaly

229.76786°

Mean motion

3.38724 °/min

Orbital period

106.28 mins

BSTAR

0.0036311

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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.
12 mins	2025-12-02 17:04:26.194Z	157.312° SSE	2025-12-02 17:10:26.194Z	34.546° NE	44.322°	2025-12-02 17:16:26.194Z	346.967° N
5 mins	2025-12-02 18:53:26.194Z	247.435° WSW	2025-12-02 18:55:26.194Z	268.016° W	15.497°	2025-12-02 18:58:26.194Z	297.771° NW
11 mins	2025-12-03 05:59:26.194Z	26.014° NE	2025-12-03 06:04:26.194Z	100.773° ESE	41.413°	2025-12-03 06:10:26.194Z	182.08° SSW
8 mins	2025-12-03 07:45:26.194Z	337.927° N	2025-12-03 07:48:26.194Z	303.767° NW	22.428°	2025-12-03 07:53:26.194Z	251.573° W

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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: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2025-12-02T05:18:26.224Z)

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: 11 hours ago