NIMBUS 2 DEB, 59973

Orbit data source: Space-Track

NIMBUS 2 DEB, 59973 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/59973?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59973, 1966-040CC

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: 18 hours ago

TLE from 18 hours ago

0 NIMBUS 2 DEB
1 59973U 66040CC  26098.39644871  .00001598  00000-0  28882-2 0  9999
2 59973 100.2431 268.4873 0042377   6.7821 353.3873 13.42548969406688

Epoch: 2026-04-08T09:30Z

TLE epoch observation values (Epoch: 2026-04-08T09:30:53.168Z)

Latitude

0.00004°

Longitude

-70.89365°

Altitude

1,071.073 km

Speed

7.332 km/s

True Right ascension

17h 53m 56s

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

10:03:12

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,128.817 km

Perigee altitude

1,065.461 km

Semi-major axis

7,475.276 km

Eccentricity

0.00424

Inclination

100.2431°

RAAN

268.4873°

Arg. of periapsis

6.7821°

True anomaly

353.33108°

Mean anomaly

353.3873°

Eccentric anomaly

353.35922°

Mean motion

3.35817 °/min

Orbital period

107.2 mins

BSTAR

0.0028882

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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.
12 mins	2026-04-09 10:40:00.882Z	144.402° SSE	2026-04-09 10:46:00.882Z	58.825° ENE	40.093°	2026-04-09 10:52:00.882Z	352.885° N
8 mins	2026-04-09 12:28:00.882Z	224.075° SW	2026-04-09 12:32:00.882Z	269.281° W	21.435°	2026-04-09 12:36:00.882Z	311.386° NW
11 mins	2026-04-09 23:41:00.882Z	30.368° NE	2026-04-09 23:46:00.882Z	92.66° ESE	37.339°	2026-04-09 23:52:00.882Z	172.739° S
10 mins	2026-04-10 01:27:00.882Z	349.672° N	2026-04-10 01:32:00.882Z	291.833° WNW	26.577°	2026-04-10 01:37:00.882Z	241.802° WSW

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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, 59973 on other resources

View NIMBUS 2 DEB, 59973 on Heavens-Above

View NIMBUS 2 DEB, 59973 on Keep Track

View NIMBUS 2 DEB, 59973 on Celestrak

View NIMBUS 2 DEB, 59973 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, 59973

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2026-04-08T09:30:53.168Z)

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, 59973 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 18 hours ago