DELTA 1 DEB (YO), 228

Orbit data source: Space-Track

DELTA 1 DEB (YO), 228 is space debris in LEO originally from a launch on Thu, 08 Feb 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/228?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

228, 1962-002C

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)

1962-02-08 (64 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)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 DELTA 1 DEB (YO)
1 00228U 62002C   26012.17067076  .00028338  00000-0  66041-3 0  9991
2 00228  48.4324  60.7036 0004934  96.5968 263.5534 15.41925917418942

Epoch: 2026-01-12T04:05Z

TLE epoch observation values (Epoch: 2026-01-12T04:05:45.953Z)

Latitude

-0.00003°

Longitude

-112.4091°

Altitude

441.189 km

Speed

7.649 km/s

True Right ascension

04h 02m 48s

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

06:35:47

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

444.83 km

Perigee altitude

438.101 km

Semi-major axis

6,819.603 km

Eccentricity

0.00049

Inclination

48.4324°

RAAN

60.7036°

Arg. of periapsis

96.5968°

True anomaly

263.49722°

Mean anomaly

263.5534°

Eccentric anomaly

263.52531°

Mean motion

3.85394 °/min

Orbital period

93.41 mins

BSTAR

0.00066041

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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

DELTA 1 DEB, 28443

DELTA 1 DEB (YO), 227

DELTA 1 R/B, 229 (Decayed)

TIROS 4, 226

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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.
6 mins	2026-01-13 06:45:18.738Z	254.818° W	2026-01-13 06:48:18.738Z	318.214° NNW	38.842°	2026-01-13 06:51:18.738Z	49.952° ENE
4 mins	2026-01-13 10:03:18.738Z	333.502° NNW	2026-01-13 10:05:18.738Z	23.622° NE	20.97°	2026-01-13 10:07:18.738Z	62.492° ENE
4 mins	2026-01-13 11:41:18.738Z	309.309° NW	2026-01-13 11:43:18.738Z	92.359° ESE	41.125°	2026-01-13 11:45:18.738Z	114.611° 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), 228 on other resources

View DELTA 1 DEB (YO), 228 on Heavens-Above

View DELTA 1 DEB (YO), 228 on Keep Track

View DELTA 1 DEB (YO), 228 on Celestrak

View DELTA 1 DEB (YO), 228 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), 228

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-01-12T04:05:45.953Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

DELTA 1 DEB (YO) Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB (YO), 228 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago