DELTA 1 DEB, 42082

Orbit data source: Space-Track

DELTA 1 DEB, 42082 is space debris in SSO originally from a launch on Sun, 15 Dec 1968 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/42082?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

42082, 1968-114J

Orbit

SSO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Aerojet

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1968-12-15 (58 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.2 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 3 days ago

0 DELTA 1 DEB
1 42082U 68114J   26170.10359353  .00000080  00000-0  89114-3 0  9995
2 42082 101.9717 118.7311 0086797 307.0490  64.6337 12.42830616570651

Epoch: 2026-06-19T02:29Z

TLE epoch observation values (Epoch: 2026-06-19T02:29:10.480Z)

Latitude

12.27213°

Longitude

171.46939°

Altitude

1,467.642 km

Speed

7.143 km/s

True Right ascension

07h 44m 24s

True Declination

12° 12' 26"

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

21:52:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,560.508 km

Perigee altitude

1,423.884 km

Semi-major axis

7,870.333 km

Eccentricity

0.00868

Inclination

101.9717°

RAAN

118.7311°

Arg. of periapsis

307.049°

True anomaly

65.53659°

Mean anomaly

64.6337°

Eccentric anomaly

65.08473°

Mean motion

3.10852 °/min

Orbital period

115.81 mins

BSTAR

0.00089114

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Other satellites on launch #114 in the year 1968 (1968-12-15 UTC)

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DELTA 1 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.
7 mins	2026-06-22 12:10:12.960Z	340.142° N	2026-06-22 12:13:12.960Z	319.171° NNW	13.879°	2026-06-22 12:17:12.960Z	290.726° WNW
14 mins	2026-06-22 19:25:12.960Z	126.884° SE	2026-06-22 19:31:12.960Z	69.613° E	35.844°	2026-06-22 19:39:12.960Z	354.279° N
14 mins	2026-06-22 21:19:12.960Z	199° SSW	2026-06-22 21:25:12.960Z	259.262° W	33.357°	2026-06-22 21:33:12.960Z	328.535° NNW
7 mins	2026-06-23 07:36:12.960Z	68.492° E	2026-06-23 07:39:12.960Z	90.439° ESE	14.169°	2026-06-23 07:43:12.960Z	118.596° SE
16 mins	2026-06-23 09:26:12.960Z	21.063° NNE	2026-06-23 09:34:12.960Z	127.783° SE	44.263°	2026-06-23 09:42:12.960Z	193.17° SSW

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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 DELTA 1 DEB, 42082 on other resources

View DELTA 1 DEB, 42082 on Heavens-Above

View DELTA 1 DEB, 42082 on Keep Track

View DELTA 1 DEB, 42082 on Celestrak

View DELTA 1 DEB, 42082 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

DELTA 1 DEB, 42082

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: 2026-06-19T02:29:10.480Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #114 in the year 1968 (1968-12-15 UTC)

DELTA 1 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB, 42082 on other resources

Documentation

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