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)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NIMBUS 2 DEB
1 40647U 66040BL  26214.99322772  .00001619  00000-0  27644-2 0  9995
2 40647 100.2795  48.5764 0040323  30.4407 329.9053 13.46226180548754

Epoch: 2026-08-02T23:50Z

TLE epoch observation values (Epoch: 2026-08-02T23:50:14.875Z)

Latitude

-0.00002°

Longitude

99.43171°

Altitude

1,062.921 km

Speed

7.333 km/s

True Right ascension

03h 14m 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

22:57:39

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,113.6 km

Perigee altitude

1,053.425 km

Semi-major axis

7,461.65 km

Eccentricity

0.00403

Inclination

100.2795°

RAAN

48.5764°

Arg. of periapsis

30.4407°

True anomaly

329.67259°

Mean anomaly

329.9053°

Eccentric anomaly

329.78905°

Mean motion

3.36737 °/min

Orbital period

106.91 mins

BSTAR

0.0027644

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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	2026-08-04 11:39:20.323Z	114.696° SE	2026-08-04 11:44:20.323Z	57.905° ENE	25.372°	2026-08-04 11:49:20.323Z	6.427° NNE
11 mins	2026-08-04 13:24:20.323Z	189.759° SSW	2026-08-04 13:29:20.323Z	265.176° W	37.157°	2026-08-04 13:35:20.323Z	333.439° NNW
8 mins	2026-08-05 00:38:20.323Z	56.019° ENE	2026-08-05 00:41:20.323Z	88.347° E	20.706°	2026-08-05 00:46:20.323Z	140.166° SSE
11 mins	2026-08-05 02:22:20.323Z	5.878° NNE	2026-08-05 02:27:20.323Z	298.372° NW	41.319°	2026-08-05 02:33:20.323Z	213.322° SW

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-08-02T23:50:14.875Z)

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: 1 day ago