DELTA 1 R/B, 2436

Orbit data source: Space-Track

DELTA 1 R/B, 2436 is space debris in SSO originally from a launch on Sun, 02 Oct 1966 UTC launched from the Air Force Western Test Range (AFWTR). 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/2436?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/2436?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2436, 1966-087B

Orbit

SSO

Last TLE update

7 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)

1966-10-02 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

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 7 hours ago

0 DELTA 1 R/B
1 02436U 66087B   25183.55314829 -.00000015  00000-0  15054-3 0  9993
2 02436 100.9880 154.0758 0065675   9.3876 350.8413 12.57659561696153

Epoch: 2025-07-02T13:16Z

TLE epoch observation values (Epoch: 2025-07-02T13:16:32.012Z)

Latitude

-0.00006°

Longitude

34.10983°

Altitude

1,384.589 km

Speed

7.19 km/s

True Right ascension

10h 16m 18s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-62.2936°

Longitude

55.98014°

Altitude

1,441.071 km

Speed

7.148 km/s

Apparent Right ascension

17h 09m 11s

Apparent Declination

-70° 34' 41"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

08:18:30

Azimuth

157.097° SSE

Elevation

-51.079°

Doppler factor

Orbital elements

Apogee altitude

1,481.394 km

Perigee altitude

1,378.832 km

Semi-major axis

7,808.25 km

Eccentricity

0.00657

Inclination

100.988°

RAAN

154.0758°

Arg. of periapsis

9.3876°

True anomaly

Unknown

Mean anomaly

350.8413°

Eccentric anomaly

Unknown

Mean motion

3.14567 °/min

Orbital period

114.44 mins

BSTAR

0.00015054

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Other satellites on launch #87 in the year 1966 (1966-10-02 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.
14 mins	2025-07-02 21:01:27.189Z	134.19° SE	2025-07-02 21:08:27.189Z	67.081° ENE	36.641°	2025-07-02 21:15:27.189Z	356.01° N
12 mins	2025-07-02 22:55:27.189Z	204.284° SW	2025-07-02 23:01:27.189Z	266.244° W	30.448°	2025-07-02 23:07:27.189Z	323.01° NNW
6 mins	2025-07-03 09:04:27.189Z	67.792° E	2025-07-03 09:07:27.189Z	90.875° ESE	14.144°	2025-07-03 09:10:27.189Z	113.374° SE
15 mins	2025-07-03 10:53:27.189Z	19.106° NNE	2025-07-03 11:00:27.189Z	76.217° E	44.452°	2025-07-03 11:08:27.189Z	193.176° SSW
11 mins	2025-07-03 12:47:27.189Z	346.977° N	2025-07-03 12:52:27.189Z	304.347° NW	22.218°	2025-07-03 12:58:27.189Z	257.069° W
9 mins	2025-07-03 20:01:27.189Z	85.591° E	2025-07-03 20:05:27.189Z	50.312° ENE	19.151°	2025-07-03 20:10:27.189Z	10.911° NNE

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Check out DELTA 1 R/B, 2436 on other resources

View DELTA 1 R/B, 2436 on Heavens-Above

View DELTA 1 R/B, 2436 on Keep Track

View DELTA 1 R/B, 2436 on Celestrak

View DELTA 1 R/B, 2436 on Gunter's Space Page

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