NIMBUS 2 DEB, 40646

Orbit data source: Space-Track

NIMBUS 2 DEB, 40646 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/40646?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40646, 1966-040BK

Orbit

SSO

Last TLE update

2 days ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-05-15 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 NIMBUS 2 DEB
1 40646U 66040BK  25180.10327463  .00001223  00000-0  20544-2 0  9993
2 40646 100.3671  55.5959 0046737 263.0133  96.5681 13.47798739496386

Epoch: 2025-06-29T02:28Z

TLE epoch observation values (Epoch: 2025-06-29T02:28:42.928Z)

Latitude

0.00006°

Longitude

100.98478°

Altitude

1,087.276 km

Speed

7.307 km/s

True Right ascension

03h 42m 23s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-52.32783°

Longitude

116.68286°

Altitude

1,077.329 km

Speed

7.324 km/s

Apparent Right ascension

03h 17m 31s

Apparent Declination

-48° 24' 60"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

13:56:07

Azimuth

232.924° WSW

Elevation

-73.186°

Doppler factor

Orbital elements

Apogee altitude

1,112.554 km

Perigee altitude

1,042.862 km

Semi-major axis

7,455.845 km

Eccentricity

0.00467

Inclination

100.3671°

RAAN

55.5959°

Arg. of periapsis

263.0133°

True anomaly

Unknown

Mean anomaly

96.5681°

Eccentric anomaly

Unknown

Mean motion

3.3713 °/min

Orbital period

106.78 mins

BSTAR

0.0020544

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Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

NIMBUS 2 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-01 03:13:01.063Z	50.843° ENE	2025-07-01 03:17:01.063Z	88.685° E	17.699°	2025-07-01 03:21:01.063Z	129.236° SE
11 mins	2025-07-01 04:58:01.063Z	9.568° NNE	2025-07-01 05:03:01.063Z	295.846° NW	43.578°	2025-07-01 05:09:01.063Z	207.077° SW
11 mins	2025-07-01 15:11:01.063Z	144.301° SSE	2025-07-01 15:16:01.063Z	52.836° ENE	41.456°	2025-07-01 15:22:01.063Z	351.335° N
8 mins	2025-07-01 16:58:01.063Z	230.313° WSW	2025-07-01 17:01:01.063Z	263.089° W	20.624°	2025-07-01 17:06:01.063Z	313.363° NW

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Check out NIMBUS 2 DEB, 40646 on other resources

View NIMBUS 2 DEB, 40646 on Heavens-Above

View NIMBUS 2 DEB, 40646 on Keep Track

View NIMBUS 2 DEB, 40646 on Celestrak

View NIMBUS 2 DEB, 40646 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.