NIMBUS 2 DEB, 59974

Orbit data source: Space-Track

NIMBUS 2 DEB, 59974 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/59974?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59974, 1966-040CD

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 59974U 66040CD  26213.19375858  .00001517  00000-0  26754-2 0  9990
2 59974 100.1416  15.0506 0041136  72.0332 288.5275 13.44223908463835

Epoch: 2026-08-01T04:39Z

TLE epoch observation values (Epoch: 2026-08-01T04:39:00.741Z)

Latitude

-0.00003°

Longitude

-4.51156°

Altitude

1,086.694 km

Speed

7.314 km/s

True Right ascension

01h 00m 12s

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

17:57:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,121.643 km

Perigee altitude

1,060.193 km

Semi-major axis

7,469.055 km

Eccentricity

0.00411

Inclination

100.1416°

RAAN

15.0506°

Arg. of periapsis

72.0332°

True anomaly

288.07982°

Mean anomaly

288.5275°

Eccentric anomaly

288.30373°

Mean motion

3.36236 °/min

Orbital period

107.07 mins

BSTAR

0.0026754

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

THOR AGENA B R/B, 2174

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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 09:35:57.425Z	118.741° SE	2026-08-04 09:40:57.425Z	64.54° ENE	26.656°	2026-08-04 09:45:57.425Z	7.963° NNE
10 mins	2026-08-04 11:21:57.425Z	194.687° SSW	2026-08-04 11:25:57.425Z	249.538° W	35.727°	2026-08-04 11:31:57.425Z	330.441° NNW
9 mins	2026-08-04 22:35:57.425Z	50.585° ENE	2026-08-04 22:39:57.425Z	95.452° ESE	22.495°	2026-08-04 22:44:57.425Z	146.14° SSE
11 mins	2026-08-05 00:20:57.425Z	2.305° NNE	2026-08-05 00:25:57.425Z	283.02° WNW	39.535°	2026-08-05 00:31:57.425Z	215.772° 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, 59974 on other resources

View NIMBUS 2 DEB, 59974 on Heavens-Above

View NIMBUS 2 DEB, 59974 on Keep Track

View NIMBUS 2 DEB, 59974 on Celestrak

View NIMBUS 2 DEB, 59974 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, 59974

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: 2026-08-01T04:39:00.741Z)

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, 59974 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago