NIMBUS 2 DEB, 59970

Orbit data source: Space-Track

NIMBUS 2 DEB, 59970 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/59970?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59970, 1966-040BZ

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 59970U 66040BZ  26256.48248883  .00000998  00000-0  18614-2 0  9990
2 59970 100.3485  81.0192 0056826   6.9907 353.2000 13.41410352436080

Epoch: 2026-09-13T11:34Z

TLE epoch observation values (Epoch: 2026-09-13T11:34:47.034Z)

Latitude

-0.00011°

Longitude

-85.15326°

Altitude

1,064.558 km

Speed

7.34 km/s

True Right ascension

05h 24m 04s

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

09:09:11

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,143.88 km

Perigee altitude

1,058.874 km

Semi-major axis

7,479.514 km

Eccentricity

0.00568

Inclination

100.3485°

RAAN

81.0192°

Arg. of periapsis

6.9907°

True anomaly

353.12235°

Mean anomaly

353.2°

Eccentric anomaly

353.16123°

Mean motion

3.35531 °/min

Orbital period

107.29 mins

BSTAR

0.0018614

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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	2026-09-17 00:19:08.076Z	37.301° NE	2026-09-17 00:25:08.076Z	100.706° ESE	30.853°	2026-09-17 00:30:08.076Z	153.187° SSE
11 mins	2026-09-17 02:06:08.076Z	357.374° N	2026-09-17 02:11:08.076Z	282.276° WNW	47.257°	2026-09-17 02:17:08.076Z	222.188° SW
6 mins	2026-09-17 10:39:08.076Z	80.997° E	2026-09-17 10:41:08.076Z	59.807° ENE	18.039°	2026-09-17 10:45:08.076Z	20.061° NNE
11 mins	2026-09-17 12:21:08.076Z	167.112° S	2026-09-17 12:26:08.076Z	220.807° SW	80.612°	2026-09-17 12:32:08.076Z	342.187° N

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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, 59970 on other resources

View NIMBUS 2 DEB, 59970 on Heavens-Above

View NIMBUS 2 DEB, 59970 on Keep Track

View NIMBUS 2 DEB, 59970 on Celestrak

View NIMBUS 2 DEB, 59970 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, 59970

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: 2026-09-13T11:34:47.034Z)

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, 59970 on other resources

Documentation

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