NIMBUS 2 DEB, 26816

Orbit data source: Space-Track

NIMBUS 2 DEB, 26816 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/26816?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26816, 1966-040L

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 (61 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 NIMBUS 2 DEB
1 26816U 66040L   26317.39367198  .00002146  00000-0  29653-2 0  9994
2 26816 100.3342 271.7697 0052475 115.3257  36.9047 13.58924357264170

Epoch: 2026-11-13T09:26Z

TLE epoch observation values (Epoch: 2026-11-13T09:26:53.259Z)

Latitude

26.96441°

Longitude

-97.17045°

Altitude

1,011.713 km

Speed

7.364 km/s

True Right ascension

06h 28m 15s

True Declination

26° 49' 50"

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

13:40:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,075.837 km

Perigee altitude

998.016 km

Semi-major axis

7,415.064 km

Eccentricity

0.00525

Inclination

100.3342°

RAAN

271.7697°

Arg. of periapsis

115.3257°

True anomaly

37.26768°

Mean anomaly

36.9047°

Eccentric anomaly

37.086°

Mean motion

3.39915 °/min

Orbital period

105.91 mins

BSTAR

0.0029653

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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.
7 mins	2026-11-13 19:28:55.416Z	95.29° ESE	2026-11-13 19:31:55.416Z	63.939° ENE	19.579°	2026-11-13 19:35:55.416Z	20.489° NNE
11 mins	2026-11-13 21:10:55.416Z	172.518° S	2026-11-13 21:15:55.416Z	240.188° WSW	71.802°	2026-11-13 21:21:55.416Z	339.68° N
10 mins	2026-11-14 10:02:55.416Z	18.544° NNE	2026-11-14 10:06:55.416Z	47.909° ENE	76.57°	2026-11-14 10:12:55.416Z	193.671° SSW
5 mins	2026-11-14 11:48:55.416Z	326.078° NNW	2026-11-14 11:50:55.416Z	304.146° NW	16.77°	2026-11-14 11:53:55.416Z	272.564° WNW

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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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Check out NIMBUS 2 DEB, 26816 on other resources

View NIMBUS 2 DEB, 26816 on Heavens-Above

View NIMBUS 2 DEB, 26816 on Keep Track

View NIMBUS 2 DEB, 26816 on Celestrak

View NIMBUS 2 DEB, 26816 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, 26816

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: 2026-11-13T09:26:53.259Z)

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, 26816 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago