NIMBUS 2 DEB, 59971

Orbit data source: Space-Track

NIMBUS 2 DEB, 59971 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/59971?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59971, 1966-040CA

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: 10 hours ago

TLE from 10 hours ago

0 NIMBUS 2 DEB
1 59971U 66040CA  26128.10277889  .00001351  00000-0  25229-2 0  9990
2 59971 100.4404 335.7344 0059763 352.4213   7.6005 13.40491252253958

Epoch: 2026-05-08T02:28Z

TLE epoch observation values (Epoch: 2026-05-08T02:28:00.096Z)

Latitude

0.00001°

Longitude

72.79462°

Altitude

1,065.85 km

Speed

7.341 km/s

True Right ascension

22h 22m 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

20:21:07

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,149.523 km

Perigee altitude

1,060.083 km

Semi-major axis

7,482.94 km

Eccentricity

0.00598

Inclination

100.4404°

RAAN

335.7344°

Arg. of periapsis

352.4213°

True anomaly

7.69176°

Mean anomaly

7.6005°

Eccentric anomaly

7.64606°

Mean motion

3.35301 °/min

Orbital period

107.37 mins

BSTAR

0.0025229

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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	2026-05-08 13:19:13.302Z	149.963° SSE	2026-05-08 13:25:13.302Z	68.838° E	42.538°	2026-05-08 13:31:13.302Z	350.601° N
7 mins	2026-05-08 15:08:13.302Z	232.042° WSW	2026-05-08 15:11:13.302Z	263.87° W	18.705°	2026-05-08 15:15:13.302Z	305.682° NW
11 mins	2026-05-09 02:22:13.302Z	29.16° NE	2026-05-09 02:27:13.302Z	107.861° ESE	40.283°	2026-05-09 02:33:13.302Z	179.473° S
9 mins	2026-05-09 04:08:13.302Z	345.393° N	2026-05-09 04:12:13.302Z	301.881° NW	24.479°	2026-05-09 04:17:13.302Z	249.508° W

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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, 59971 on other resources

View NIMBUS 2 DEB, 59971 on Heavens-Above

View NIMBUS 2 DEB, 59971 on Keep Track

View NIMBUS 2 DEB, 59971 on Celestrak

View NIMBUS 2 DEB, 59971 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, 59971

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: 2026-05-08T02:28:00.096Z)

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, 59971 on other resources

Documentation

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