NIMBUS 2 DEB, 26669

Orbit data source: Space-Track

NIMBUS 2 DEB, 26669 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/26669?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26669, 1966-040J

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: 21 hours ago

TLE from 21 hours ago

0 NIMBUS 2 DEB
1 26669U 66040J   25335.82672117  .00005951  00000-0  51177-2 0  9990
2 26669 100.1345   2.7965 0033343 326.8073 212.1427 13.86814356262474

Epoch: 2025-12-01T19:50Z

TLE epoch observation values (Epoch: 2025-12-01T19:50:28.709Z)

Latitude

1.12647°

Longitude

174.45657°

Altitude

963.184 km

Speed

7.36 km/s

True Right ascension

12h 11m 59s

True Declination

1° 07' 12"

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

15:00:08

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

961.483 km

Perigee altitude

912.701 km

Semi-major axis

7,315.229 km

Eccentricity

0.00333

Inclination

100.1345°

RAAN

2.7965°

Arg. of periapsis

326.8073°

True anomaly

211.94014°

Mean anomaly

212.1427°

Eccentric anomaly

212.04135°

Mean motion

3.46898 °/min

Orbital period

103.78 mins

BSTAR

0.0051177

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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.
8 mins	2025-12-03 00:34:25.217Z	105.608° ESE	2025-12-03 00:38:25.217Z	57.616° ENE	21.147°	2025-12-03 00:42:25.217Z	13.253° NNE
10 mins	2025-12-03 02:15:25.217Z	183.199° SSW	2025-12-03 02:20:25.217Z	270.369° WNW	39.27°	2025-12-03 02:25:25.217Z	334.478° NNW
11 mins	2025-12-03 14:50:25.217Z	17.491° NNE	2025-12-03 14:56:25.217Z	116.557° SE	44.597°	2025-12-03 15:01:25.217Z	192.088° SSW
6 mins	2025-12-03 16:35:25.217Z	330.465° NNW	2025-12-03 16:38:25.217Z	296.897° NW	16.007°	2025-12-03 16:41:25.217Z	266.293° 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, 26669 on other resources

View NIMBUS 2 DEB, 26669 on Heavens-Above

View NIMBUS 2 DEB, 26669 on Keep Track

View NIMBUS 2 DEB, 26669 on Celestrak

View NIMBUS 2 DEB, 26669 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, 26669

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 21 hours ago

TLE from 21 hours ago

TLE epoch observation values (Epoch: 2025-12-01T19:50:28.709Z)

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, 26669 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 21 hours ago