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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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 (63 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

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Last TLE update: 17 hours ago

TLE from 17 hours ago

0 DELTA 1 DEB (YO)
1 00312U 62025C   25341.76302657  .00001859  00000-0  31816-3 0  9997
2 00312  58.2465   6.5092 0196292  50.8456 310.9835 14.61274832330932

Epoch: 2025-12-07T18:18Z

TLE epoch observation values (Epoch: 2025-12-07T18:18:45.495Z)

Latitude

-0.00005°

Longitude

15.04786°

Altitude

601.044 km

Speed

7.608 km/s

True Right ascension

00h 26m 02s

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

09:12:55

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

827.251 km

Perigee altitude

549.825 km

Semi-major axis

7,066.675 km

Eccentricity

0.01963

Inclination

58.2465°

RAAN

6.5092°

Arg. of periapsis

50.8456°

True anomaly

309.25798°

Mean anomaly

310.9835°

Eccentric anomaly

310.12351°

Mean motion

3.6536 °/min

Orbital period

98.53 mins

BSTAR

0.00031816

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

DELTA 1 DEB (YO), 313 (Decayed)

DELTA 1 DEB, 6251 (Decayed)

DELTA 1 R/B, 311 (Decayed)

TIROS 5, 309

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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.
8 mins	2025-12-08 11:13:33.570Z	335.309° NNW	2025-12-08 11:17:33.570Z	58.137° ENE	32.261°	2025-12-08 11:21:33.570Z	112.216° ESE
6 mins	2025-12-08 12:56:33.570Z	283.472° WNW	2025-12-08 12:59:33.570Z	226.187° WSW	25.471°	2025-12-08 13:02:33.570Z	183.149° SSW
6 mins	2025-12-09 03:18:33.570Z	182.802° SSW	2025-12-09 03:20:33.570Z	138.437° SSE	31.298°	2025-12-09 03:24:33.570Z	57.385° ENE
4 mins	2025-12-09 05:01:33.570Z	289.508° WNW	2025-12-09 05:02:33.570Z	310.861° NW	22.734°	2025-12-09 05:05:33.570Z	11.386° NNE
5 mins	2025-12-09 10:12:33.570Z	0.2° NNE	2025-12-09 10:14:33.570Z	34.875° NE	19.698°	2025-12-09 10:17:33.570Z	79.324° E

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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 (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: 2025-12-07T18:18:45.495Z)

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