NIMBUS 2 DEB, 40641

Orbit data source: Space-Track

NIMBUS 2 DEB, 40641 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/40641?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40641, 1966-040BE

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: 2 days ago

TLE from 2 days ago

0 NIMBUS 2 DEB
1 40641U 66040BE  26133.63675881  .00001183  00000-0  20709-2 0  9993
2 40641 100.4070  22.5769 0044330 276.0033  83.6045 13.45292023538266

Epoch: 2026-05-13T15:16Z

TLE epoch observation values (Epoch: 2026-05-13T15:16:55.961Z)

Latitude

-0.00003°

Longitude

-78.0502°

Altitude

1,088.841 km

Speed

7.31 km/s

True Right ascension

01h 30m 18s

True Declination

0° 00' 00"

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

06:34:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,120.069 km

Perigee altitude

1,053.883 km

Semi-major axis

7,465.113 km

Eccentricity

0.00443

Inclination

100.407°

RAAN

22.5769°

Arg. of periapsis

276.0033°

True anomaly

84.10963°

Mean anomaly

83.6045°

Eccentric anomaly

83.85703°

Mean motion

3.36503 °/min

Orbital period

106.98 mins

BSTAR

0.0020709

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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.
11 mins	2026-05-16 04:35:11.692Z	38.314° NE	2026-05-16 04:40:11.692Z	92.461° ESE	28.395°	2026-05-16 04:46:11.692Z	158.506° S
10 mins	2026-05-16 06:21:11.692Z	356.958° N	2026-05-16 06:26:11.692Z	288.194° WNW	34.689°	2026-05-16 06:31:11.692Z	228.718° WSW
7 mins	2026-05-16 14:52:11.692Z	87.295° E	2026-05-16 14:55:11.692Z	55.47° ENE	18.723°	2026-05-16 14:59:11.692Z	16.879° NNE
12 mins	2026-05-16 16:34:11.692Z	168.979° S	2026-05-16 16:40:11.692Z	298.664° NW	43.907°	2026-05-16 16:46:11.692Z	341.601° 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, 40641 on other resources

View NIMBUS 2 DEB, 40641 on Heavens-Above

View NIMBUS 2 DEB, 40641 on Keep Track

View NIMBUS 2 DEB, 40641 on Celestrak

View NIMBUS 2 DEB, 40641 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, 40641

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-05-13T15:16:55.961Z)

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, 40641 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago