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 (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: 10 hours ago

TLE from 10 hours ago

0 NIMBUS 2 DEB
1 26816U 66040L   26033.30319740  .00002540  00000-0  35636-2 0  9996
2 26816 100.3473 332.8574 0055988  91.2216  62.2316 13.57685900225600

Epoch: 2026-02-02T07:16Z

TLE epoch observation values (Epoch: 2026-02-02T07:16:36.255Z)

Latitude

25.5563°

Longitude

-83.81127°

Altitude

1,027.903 km

Speed

7.35 km/s

True Right ascension

10h 31m 21s

True Declination

25° 25' 39"

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

19:12:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,082.98 km

Perigee altitude

999.899 km

Semi-major axis

7,419.576 km

Eccentricity

0.0056

Inclination

100.3473°

RAAN

332.8574°

Arg. of periapsis

91.2216°

True anomaly

62.80114°

Mean anomaly

62.2316°

Eccentric anomaly

62.51618°

Mean motion

3.39605 °/min

Orbital period

106.01 mins

BSTAR

0.0035636

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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.
10 mins	2026-02-02 19:02:05.446Z	134.042° SE	2026-02-02 19:07:05.446Z	66.8° ENE	35.443°	2026-02-02 19:12:05.446Z	359.907° N
8 mins	2026-02-02 20:48:05.446Z	216.917° SW	2026-02-02 20:52:05.446Z	269.668° W	25.264°	2026-02-02 20:56:05.446Z	315.839° NNW
9 mins	2026-02-03 07:55:05.446Z	48.983° ENE	2026-02-03 07:59:05.446Z	106.269° ESE	27.485°	2026-02-03 08:04:05.446Z	158.833° S
9 mins	2026-02-03 09:39:05.446Z	353.163° N	2026-02-03 09:43:05.446Z	294.969° NW	33.226°	2026-02-03 09:48:05.446Z	229.962° WSW

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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, 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: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-02-02T07:16:36.255Z)

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: 10 hours ago