DELTA 1 R/B, 341

Orbit data source: Space-Track

DELTA 1 R/B, 341 is space debris in LEO originally from a launch on Tue, 10 Jul 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 src="https://www.satcat.com/sats-embedded/341?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/341?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

341, 1962-029B

Orbit

LEO

Last TLE update

1 day ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

ABL

Mission

Spacecraft

Bus & Motor

ALTAIR, Unknown motor

Mass

24 kg wet, 24 kg dry

Launch date (UTC)

1962-07-10 (63 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 0.8 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 1 day ago

0 DELTA 1 R/B
1 00341U 62029B   25220.87084890 -.00000100  00000-0 -48622-3 0  9990
2 00341  44.7907  78.5471 2423317 357.9861   9.7516  9.14314635106566

Epoch: 2025-08-08T20:54Z

TLE epoch observation values (Epoch: 2025-08-08T20:54:01.344Z)

Latitude

10.08632°

Longitude

177.69287°

Altitude

999.351 km

Speed

8.175 km/s

True Right ascension

05h 55m 15s

True Declination

10° 01' 45"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-44.65561°

Longitude

83.15115°

Altitude

2,527.703 km

Speed

6.953 km/s

Apparent Right ascension

00h 10m 25s

Apparent Declination

-42° 54' 46"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

12:53:40

Azimuth

113.805° SE

Elevation

-81.361°

Doppler factor

Orbital elements

Apogee altitude

5,625.142 km

Perigee altitude

942.375 km

Semi-major axis

9,661.895 km

Eccentricity

0.24233

Inclination

44.7907°

RAAN

78.5471°

Arg. of periapsis

357.9861°

True anomaly

16.39319°

Mean anomaly

9.7516°

Eccentric anomaly

12.83628°

Mean motion

2.28533 °/min

Orbital period

157.53 mins

BSTAR

-0.00048622

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Other satellites on launch #29 in the year 1962 (1962-07-10 UTC)

TELSTAR 1, 340

DELTA 1 R/B Visibility forecast

Observer location: undefined°, undefined°

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.
49 mins	2025-08-09 23:30:27.711Z	293.401° NW	2025-08-09 23:46:27.711Z	216.698° SW	44.598°	2025-08-10 00:19:27.711Z	130.558° SE
49 mins	2025-08-10 02:19:27.711Z	288.085° WNW	2025-08-10 02:38:27.711Z	233.306° WSW	32.083°	2025-08-10 03:08:27.711Z	175.352° S
20 mins	2025-08-10 17:36:27.711Z	225.7° WSW	2025-08-10 17:42:27.711Z	146.027° SSE	43.195°	2025-08-10 17:56:27.711Z	65.868° ENE
32 mins	2025-08-10 20:21:27.711Z	277.204° WNW	2025-08-10 20:30:27.711Z	359.692° N	43.756°	2025-08-10 20:53:27.711Z	87.061° E

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 R/B, 341 on other resources

View DELTA 1 R/B, 341 on Heavens-Above

View DELTA 1 R/B, 341 on Keep Track

View DELTA 1 R/B, 341 on Celestrak

View DELTA 1 R/B, 341 on Gunter's Space Page

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