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, 0.091 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 NIMBUS 2 DEB
1 40648U 66040BM  26305.82112179  .00001817  00000-0  28993-2 0  9995
2 40648 100.1976 140.1027 0033039 150.7329 209.5663 13.50459427561629

Epoch: 2026-11-01T19:42Z

TLE epoch observation values (Epoch: 2026-11-01T19:42:24.922Z)

Latitude

-0.00006°

Longitude

163.39187°

Altitude

1,094.766 km

Speed

7.294 km/s

True Right ascension

09h 20m 24s

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

00:58:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,092.497 km

Perigee altitude

1,043.295 km

Semi-major axis

7,446.033 km

Eccentricity

0.0033

Inclination

100.1976°

RAAN

140.1027°

Arg. of periapsis

150.7329°

True anomaly

209.38016°

Mean anomaly

209.5663°

Eccentric anomaly

209.47316°

Mean motion

3.37797 °/min

Orbital period

106.57 mins

BSTAR

0.0028993

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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	2026-11-02 11:50:34.434Z	120.335° SE	2026-11-02 11:55:34.434Z	69.991° E	30.375°	2026-11-02 12:01:34.434Z	4.593° NNE
11 mins	2026-11-02 13:35:34.434Z	190.563° SSW	2026-11-02 13:40:34.434Z	253.797° W	46.985°	2026-11-02 13:46:34.434Z	330.969° NNW
8 mins	2026-11-03 00:47:34.434Z	51.958° ENE	2026-11-03 00:51:34.434Z	96.322° ESE	22.136°	2026-11-03 00:55:34.434Z	138.745° SSE
11 mins	2026-11-03 02:31:34.434Z	5.336° NNE	2026-11-03 02:36:34.434Z	300.423° NW	58.581°	2026-11-03 02:42:34.434Z	214.289° 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, 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: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-11-01T19:42:24.922Z)

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: 10 hours ago