NIMBUS 2 DEB, 40648

Orbit data source: Space-Track

NIMBUS 2 DEB, 40648 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/40648?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40648, 1966-040BM

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: 11 hours ago

TLE from 11 hours ago

0 NIMBUS 2 DEB
1 40648U 66040BM  26079.04121077  .00002133  00000-0  34408-2 0  9994
2 40648 100.2065 267.9648 0037572 340.2535  19.7140 13.49475954531020

Epoch: 2026-03-20T00:59Z

TLE epoch observation values (Epoch: 2026-03-20T00:59:20.610Z)

Latitude

-0.00011°

Longitude

75.54697°

Altitude

1,050.603 km

Speed

7.34 km/s

True Right ascension

17h 51m 51s

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

17:20:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,099.506 km

Perigee altitude

1,043.526 km

Semi-major axis

7,449.653 km

Eccentricity

0.00376

Inclination

100.2065°

RAAN

267.9648°

Arg. of periapsis

340.2535°

True anomaly

19.85988°

Mean anomaly

19.714°

Eccentric anomaly

19.78687°

Mean motion

3.37551 °/min

Orbital period

106.65 mins

BSTAR

0.0034408

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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	2026-03-20 13:33:00.022Z	211.594° SW	2026-03-20 13:38:00.022Z	266.39° W	24.058°	2026-03-20 13:43:00.022Z	318.919° NNW
11 mins	2026-03-21 00:44:00.022Z	34.888° NE	2026-03-21 00:49:00.022Z	96.227° ESE	33.116°	2026-03-21 00:55:00.022Z	166.404° S
10 mins	2026-03-21 02:30:00.022Z	349.209° N	2026-03-21 02:34:00.022Z	297.773° NW	30.265°	2026-03-21 02:40:00.022Z	233.051° WSW
7 mins	2026-03-21 10:59:00.022Z	90.758° ESE	2026-03-21 11:02:00.022Z	55.543° ENE	20.471°	2026-03-21 11:06:00.022Z	14.964° NNE

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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, 40648 on other resources

View NIMBUS 2 DEB, 40648 on Heavens-Above

View NIMBUS 2 DEB, 40648 on Keep Track

View NIMBUS 2 DEB, 40648 on Celestrak

View NIMBUS 2 DEB, 40648 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, 40648

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-03-20T00:59:20.610Z)

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, 40648 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago