DELTA 1 R/B, 2096

Orbit data source: Space-Track

DELTA 1 R/B, 2096 is space debris in SSO originally from a launch on Mon, 28 Feb 1966 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/2096?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/2096?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2096, 1966-016B

Orbit

SSO

Last TLE update

22 hours ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

ABL

Mission

Spacecraft

Bus & Motor

ALTAIR, Unknown motor

Mass

33 kg wet, 33 kg dry

Launch date (UTC)

1966-02-28 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.5 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 22 hours ago

0 DELTA 1 R/B
1 02096U 66016B   25181.84200509 -.00000030  00000-0  59390-4 0  9995
2 02096 100.9096  33.1300 0039904 164.8181 206.1547 12.69978389749476

Epoch: 2025-06-30T20:12Z

TLE epoch observation values (Epoch: 2025-06-30T20:12:29.239Z)

Latitude

10.52882°

Longitude

168.81934°

Altitude

1,411.74 km

Speed

7.143 km/s

True Right ascension

02h 04m 20s

True Declination

10° 28' 21"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

22.01955°

Longitude

-3.83743°

Altitude

1,353.627 km

Speed

7.198 km/s

Apparent Right ascension

15h 42m 56s

Apparent Declination

-6° 01' 10"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

05:26:10

Azimuth

41.232° NE

Elevation

-48.934°

Doppler factor

Orbital elements

Apogee altitude

1,410.457 km

Perigee altitude

1,348.544 km

Semi-major axis

7,757.638 km

Eccentricity

0.00399

Inclination

100.9096°

RAAN

33.13°

Arg. of periapsis

164.8181°

True anomaly

Unknown

Mean anomaly

206.1547°

Eccentric anomaly

Unknown

Mean motion

3.1765 °/min

Orbital period

113.33 mins

BSTAR

0.00005939

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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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.
6 mins	2025-07-02 01:12:31.287Z	64.485° ENE	2025-07-02 01:15:31.287Z	88.731° E	14.151°	2025-07-02 01:18:31.287Z	113.133° SE
14 mins	2025-07-02 03:01:31.287Z	18.047° NNE	2025-07-02 03:08:31.287Z	163.89° S	44.554°	2025-07-02 03:15:31.287Z	195.582° SSW
9 mins	2025-07-02 04:54:31.287Z	341.76° N	2025-07-02 04:58:31.287Z	306.271° NW	19.933°	2025-07-02 05:03:31.287Z	263.824° W
9 mins	2025-07-02 12:03:31.287Z	85.83° E	2025-07-02 12:07:31.287Z	51.199° ENE	18.842°	2025-07-02 12:12:31.287Z	11.628° NNE
14 mins	2025-07-02 13:51:31.287Z	160.592° S	2025-07-02 13:57:31.287Z	136.409° SSE	44.95°	2025-07-02 14:05:31.287Z	344.213° N
8 mins	2025-07-02 15:46:31.287Z	240.552° WSW	2025-07-02 15:49:31.287Z	265.058° W	16.532°	2025-07-02 15:54:31.287Z	305.358° NW

Authenticating...

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Check out DELTA 1 R/B, 2096 on other resources

View DELTA 1 R/B, 2096 on Heavens-Above

View DELTA 1 R/B, 2096 on Keep Track

View DELTA 1 R/B, 2096 on Celestrak

View DELTA 1 R/B, 2096 on Gunter's Space Page

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