DELTA 1 DEB (YO), 312

Orbit data source: Space-Track

DELTA 1 DEB (YO), 312 is space debris in LEO originally from a launch on Tue, 19 Jun 1962 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/312?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

312, 1962-025C

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)

1962-06-19 (64 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

CABLE + BOX, 0.066 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago

0 DELTA 1 DEB (YO)
1   312U 62025C   26306.82626396  .00000400  00000-0  93941-4 0  9994
2   312  58.2452 236.2364 0193969 130.4562 231.3565 14.62103611379197

Epoch: 2026-11-02T19:49Z

TLE epoch observation values (Epoch: 2026-11-02T19:49:49.206Z)

Latitude

0.00001°

Longitude

-103.31633°

Altitude

774.946 km

Speed

7.421 km/s

True Right ascension

15h 44m 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

08:21:39

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

822.887 km

Perigee altitude

548.847 km

Semi-major axis

7,064.004 km

Eccentricity

0.0194

Inclination

58.2452°

RAAN

236.2364°

Arg. of periapsis

130.4562°

True anomaly

229.64661°

Mean anomaly

231.3565°

Eccentric anomaly

230.49896°

Mean motion

3.65567 °/min

Orbital period

98.48 mins

BSTAR

0.000093941

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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

TIROS 5, 309

DELTA 1 DEB (YO), 313 (Decayed)

DELTA 1 R/B, 311 (Decayed)

DELTA 1 DEB, 6251 (Decayed)

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DELTA 1 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.
7 mins	2026-11-03 20:35:00.174Z	171.585° S	2026-11-03 20:38:00.174Z	126.92° SE	26.569°	2026-11-03 20:42:00.174Z	66.712° ENE
7 mins	2026-11-03 22:17:00.174Z	252.275° W	2026-11-03 22:20:00.174Z	312.258° NW	44.302°	2026-11-03 22:24:00.174Z	27.982° NE
7 mins	2026-11-04 05:11:00.174Z	325.379° NNW	2026-11-04 05:14:00.174Z	43.372° NE	68.353°	2026-11-04 05:18:00.174Z	130.496° SE

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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 DELTA 1 DEB (YO), 312 on other resources

View DELTA 1 DEB (YO), 312 on Heavens-Above

View DELTA 1 DEB (YO), 312 on Keep Track

View DELTA 1 DEB (YO), 312 on Celestrak

View DELTA 1 DEB (YO), 312 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 (YO), 312

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-11-02T19:49:49.206Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

DELTA 1 DEB (YO) Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB (YO), 312 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago