NIMBUS 2 DEB, 40647

Orbit data source: Space-Track

NIMBUS 2 DEB, 40647 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/40647?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40647, 1966-040BL

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 40647U 66040BL  26086.47391171  .00002055  00000-0  35185-2 0  9998
2 40647 100.2820 276.9756 0038223 340.1620  19.8022 13.45727506531463

Epoch: 2026-03-27T11:22Z

TLE epoch observation values (Epoch: 2026-03-27T11:22:25.971Z)

Latitude

-0.00002°

Longitude

-78.5406°

Altitude

1,063.936 km

Speed

7.333 km/s

True Right ascension

18h 27m 54s

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

12:55:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,113.885 km

Perigee altitude

1,056.83 km

Semi-major axis

7,463.494 km

Eccentricity

0.00382

Inclination

100.282°

RAAN

276.9756°

Arg. of periapsis

340.162°

True anomaly

19.95125°

Mean anomaly

19.8022°

Eccentric anomaly

19.87666°

Mean motion

3.36612 °/min

Orbital period

106.95 mins

BSTAR

0.0035185

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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	2026-03-29 11:40:22.590Z	131.025° SE	2026-03-29 11:46:22.590Z	56.441° ENE	32.964°	2026-03-29 11:51:22.590Z	1.069° NNE
9 mins	2026-03-29 13:27:22.590Z	209.588° SW	2026-03-29 13:31:22.590Z	262.359° W	29.174°	2026-03-29 13:36:22.590Z	321.505° NNW
10 mins	2026-03-30 00:40:22.590Z	44.899° NE	2026-03-30 00:44:22.590Z	94.715° ESE	28.911°	2026-03-30 00:50:22.590Z	159.483° S
10 mins	2026-03-30 02:25:22.590Z	355.585° N	2026-03-30 02:30:22.590Z	284.453° WNW	34.21°	2026-03-30 02:35:22.590Z	228.563° 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, 40647 on other resources

View NIMBUS 2 DEB, 40647 on Heavens-Above

View NIMBUS 2 DEB, 40647 on Keep Track

View NIMBUS 2 DEB, 40647 on Celestrak

View NIMBUS 2 DEB, 40647 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, 40647

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: 2026-03-27T11:22:25.971Z)

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, 40647 on other resources

Documentation

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