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: 5 days ago

TLE from 5 days ago

0 NIMBUS 2 DEB
1 26670U 66040K   26168.12352771  .00004515  00000-0  31365-2 0  9993
2 26670 100.2892   4.9255 0035045  71.7180  56.3363 13.99118934950593

Epoch: 2026-06-17T02:57Z

TLE epoch observation values (Epoch: 2026-06-17T02:57:52.794Z)

Latitude

50.56267°

Longitude

-112.24744°

Altitude

890.765 km

Speed

7.419 km/s

True Right ascension

13h 10m 25s

True Declination

50° 23' 49"

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

00:51:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

919.601 km

Perigee altitude

868.63 km

Semi-major axis

7,272.253 km

Eccentricity

0.0035

Inclination

100.2892°

RAAN

4.9255°

Arg. of periapsis

71.718°

True anomaly

56.67135°

Mean anomaly

56.3363°

Eccentric anomaly

56.50375°

Mean motion

3.49977 °/min

Orbital period

102.86 mins

BSTAR

0.0031365

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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.
4 mins	2026-06-22 14:38:57.516Z	244.614° WSW	2026-06-22 14:40:57.516Z	266.526° W	12.734°	2026-06-22 14:42:57.516Z	288.859° WNW
8 mins	2026-06-23 01:24:57.516Z	44.813° NE	2026-06-23 01:27:57.516Z	89.08° E	29.4°	2026-06-23 01:32:57.516Z	160.678° S
8 mins	2026-06-23 03:05:57.516Z	349.664° N	2026-06-23 03:09:57.516Z	290.957° WNW	28.424°	2026-06-23 03:13:57.516Z	237.891° WSW
9 mins	2026-06-23 12:56:57.516Z	156.757° SSE	2026-06-23 13:00:57.516Z	32.143° NE	44.232°	2026-06-23 13:05:57.516Z	347.043° N

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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: 5 days ago

TLE from 5 days ago

TLE epoch observation values (Epoch: 2026-06-17T02:57:52.794Z)

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: 5 days ago