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: 8 hours ago

TLE from 8 hours ago

0 NIMBUS 2 DEB
1 26669U 66040J   26079.38936374  .00004105  00000-0  34647-2 0  9998
2 26669 100.1202 120.3705 0032342  62.4202 313.7208 13.88144942277537

Epoch: 2026-03-20T09:20Z

TLE epoch observation values (Epoch: 2026-03-20T09:20:41.027Z)

Latitude

15.59925°

Longitude

159.43299°

Altitude

920.971 km

Speed

7.401 km/s

True Right ascension

07h 50m 06s

True Declination

15° 30' 45"

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

22:29:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

956.056 km

Perigee altitude

908.768 km

Semi-major axis

7,310.549 km

Eccentricity

0.00323

Inclination

100.1202°

RAAN

120.3705°

Arg. of periapsis

62.4202°

True anomaly

313.4522°

Mean anomaly

313.7208°

Eccentric anomaly

313.58658°

Mean motion

3.47231 °/min

Orbital period

103.68 mins

BSTAR

0.0034647

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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.
5 mins	2026-03-21 01:01:21.854Z	87.729° E	2026-03-21 01:04:21.854Z	53.148° ENE	15.752°	2026-03-21 01:06:21.854Z	30.475° NE
9 mins	2026-03-21 02:41:21.854Z	171.164° S	2026-03-21 02:45:21.854Z	234.298° WSW	44.059°	2026-03-21 02:50:21.854Z	340.38° N
10 mins	2026-03-21 15:16:21.854Z	27.447° NE	2026-03-21 15:20:21.854Z	82.054° E	39.549°	2026-03-21 15:26:21.854Z	180.524° SSW
6 mins	2026-03-21 17:00:21.854Z	329.412° NNW	2026-03-21 17:02:21.854Z	303.336° NW	20.424°	2026-03-21 17:06:21.854Z	255.64° 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: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-03-20T09:20:41.027Z)

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: 8 hours ago