THOR ABLE DEB (YO), 115

Orbit data source: Space-Track

THOR ABLE DEB (YO), 115 is space debris in LEO originally from a launch on Fri, 01 Apr 1960 UTC launched from the Air Force Eastern Test Range (AFETR). 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/115?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

115, 1960-002D

Orbit

LEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

RCA/East Windsor

Mission

Spacecraft

Bus & Motor

Unknown

Mass

~1 kg wet, ~1 kg dry

Launch date (UTC)

1960-04-01 (67 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

CABLE + BOX, 0.065 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 THOR ABLE DEB (YO)
1 00115U 60002D   26318.06210803  .00003457  00000-0  30131-3 0  9995
2 00115  48.1618  83.0890 0026182 215.8979 144.0182 14.98893616540616

Epoch: 2026-11-14T01:29Z

TLE epoch observation values (Epoch: 2026-11-14T01:29:26.133Z)

Latitude

0.00003°

Longitude

7.55785°

Altitude

585.397 km

Speed

7.561 km/s

True Right ascension

05h 32m 21s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

09:45:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

589.574 km

Perigee altitude

553.184 km

Semi-major axis

6,949.516 km

Eccentricity

0.00262

Inclination

48.1618°

RAAN

83.089°

Arg. of periapsis

215.8979°

True anomaly

144.19401°

Mean anomaly

144.0182°

Eccentric anomaly

144.10615°

Mean motion

3.74638 °/min

Orbital period

96.09 mins

BSTAR

0.00030131

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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

THOR ABLE R/B, 28 (Decayed)

THOR ABLE DEB (YO), 101 (Decayed)

TIROS 1, 29

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THOR ABLE DEB (YO) 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.
6 mins	2026-11-14 14:38:09.167Z	306.335° NW	2026-11-14 14:41:09.167Z	359.435° N	26.791°	2026-11-14 14:44:09.167Z	51.798° ENE
6 mins	2026-11-14 16:20:09.167Z	322.798° NNW	2026-11-14 16:22:09.167Z	10.053° NNE	39.2°	2026-11-14 16:26:09.167Z	87.657° E
7 mins	2026-11-14 18:00:09.167Z	288.578° WNW	2026-11-14 18:03:09.167Z	207.347° SW	54.509°	2026-11-14 18:07:09.167Z	139.173° SSE
7 mins	2026-11-15 11:17:09.167Z	225.268° WSW	2026-11-15 11:20:09.167Z	153.448° SSE	68.179°	2026-11-15 11:24:09.167Z	63.762° ENE
6 mins	2026-11-15 12:58:09.167Z	284.569° WNW	2026-11-15 13:01:09.167Z	349.782° N	36.015°	2026-11-15 13:04:09.167Z	45.82° ENE

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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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Check out THOR ABLE DEB (YO), 115 on other resources

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THOR ABLE DEB (YO), 115

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-11-14T01:29:26.133Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

THOR ABLE DEB (YO) Visibility forecast

Co-orbital & Co-planar RSOs

Check out THOR ABLE DEB (YO), 115 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago