NIMBUS 2 DEB, 26670

Orbit data source: Space-Track

NIMBUS 2 DEB, 26670 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/26670?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26670, 1966-040K

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: 13 hours ago

TLE from 13 hours ago

0 NIMBUS 2 DEB
1 26670U 66040K   26259.06214461  .00004508  00000-0  30920-2 0  9998
2 26670 100.2853 107.0071 0027556 194.2201 318.2034 13.99950335963312

Epoch: 2026-09-16T01:29Z

TLE epoch observation values (Epoch: 2026-09-16T01:29:29.294Z)

Latitude

27.34443°

Longitude

-85.02795°

Altitude

882.315 km

Speed

7.421 km/s

True Right ascension

19h 29m 27s

True Declination

27° 12' 24"

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

06:46:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

911.265 km

Perigee altitude

871.202 km

Semi-major axis

7,269.371 km

Eccentricity

0.00276

Inclination

100.2853°

RAAN

107.0071°

Arg. of periapsis

194.2201°

True anomaly

317.9924°

Mean anomaly

318.2034°

Eccentric anomaly

318.09796°

Mean motion

3.50185 °/min

Orbital period

102.8 mins

BSTAR

0.003092

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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	2026-09-16 14:35:41.227Z	197.738° SSW	2026-09-16 14:40:41.227Z	269.347° W	36.423°	2026-09-16 14:44:41.227Z	322.403° NNW
9 mins	2026-09-17 03:05:41.227Z	12.234° NNE	2026-09-17 03:09:41.227Z	249.878° W	79.118°	2026-09-17 03:14:41.227Z	201.234° SSW
8 mins	2026-09-17 12:56:41.227Z	113.005° SE	2026-09-17 12:59:41.227Z	67.855° E	32.472°	2026-09-17 13:04:41.227Z	4.702° 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, 26670 on other resources

View NIMBUS 2 DEB, 26670 on Heavens-Above

View NIMBUS 2 DEB, 26670 on Keep Track

View NIMBUS 2 DEB, 26670 on Celestrak

View NIMBUS 2 DEB, 26670 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, 26670

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-09-16T01:29:29.294Z)

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, 26670 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 13 hours ago