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: 3 days ago

TLE from 3 days ago

0 NIMBUS 2 DEB
1 40647U 66040BL  26133.01096594  .00001699  00000-0  29137-2 0  9995
2 40647 100.2807 324.6241 0037914 226.2455 133.5535 13.45931091537728

Epoch: 2026-05-13T00:15Z

TLE epoch observation values (Epoch: 2026-05-13T00:15:47.457Z)

Latitude

0.00002°

Longitude

89.89924°

Altitude

1,109.588 km

Speed

7.288 km/s

True Right ascension

21h 38m 29s

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

07:43:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,112.898 km

Perigee altitude

1,056.31 km

Semi-major axis

7,462.741 km

Eccentricity

0.00379

Inclination

100.2807°

RAAN

324.6241°

Arg. of periapsis

226.2455°

True anomaly

133.86734°

Mean anomaly

133.5535°

Eccentric anomaly

133.71052°

Mean motion

3.36663 °/min

Orbital period

106.93 mins

BSTAR

0.0029137

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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.
8 mins	2026-05-16 00:15:48.499Z	51.988° ENE	2026-05-16 00:19:48.499Z	90.824° ESE	17.517°	2026-05-16 00:23:48.499Z	130.8° SE
11 mins	2026-05-16 02:00:48.499Z	9.303° NNE	2026-05-16 02:05:48.499Z	292.99° NW	43.505°	2026-05-16 02:11:48.499Z	207.057° SW
12 mins	2026-05-16 12:13:48.499Z	147.133° SSE	2026-05-16 12:19:48.499Z	48.557° ENE	41.485°	2026-05-16 12:25:48.499Z	351.131° N
8 mins	2026-05-16 14:01:48.499Z	230.281° WSW	2026-05-16 14:04:48.499Z	262.501° W	20.475°	2026-05-16 14:09:48.499Z	312.832° NW

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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: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-05-13T00:15:47.457Z)

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: 3 days ago