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 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

20 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, 0.8 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 20 hours ago

0 DELTA 1 R/B
1 02436U 66087B   25198.50808695 -.00000025  00000-0  95342-4 0  9993
2 02436 100.9892 168.0434 0065304 339.4629  20.3826 12.57660137698031

Epoch: 2025-07-17T12:11Z

TLE epoch observation values (Epoch: 2025-07-17T12:11:38.712Z)

Latitude

-0.00004°

Longitude

49.55921°

Altitude

1,387.449 km

Speed

7.188 km/s

True Right ascension

11h 12m 10s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

67.62082°

Longitude

-101.68658°

Altitude

1,478.057 km

Speed

7.115 km/s

Apparent Right ascension

06h 11m 14s

Apparent Declination

34° 12' 00"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

20:36:57

Azimuth

29.787° NE

Elevation

-8.61°

Doppler factor

Orbital elements

Apogee altitude

1,481.102 km

Perigee altitude

1,379.12 km

Semi-major axis

7,808.248 km

Eccentricity

0.00653

Inclination

100.9892°

RAAN

168.0434°

Arg. of periapsis

339.4629°

True anomaly

20.64524°

Mean anomaly

20.3826°

Eccentric anomaly

20.51372°

Mean motion

3.14567 °/min

Orbital period

114.44 mins

BSTAR

0.000095342

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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	2025-07-18 09:49:54.946Z	35.757° NE	2025-07-18 09:56:54.946Z	97.274° ESE	29.766°	2025-07-18 10:03:54.946Z	157.957° S
14 mins	2025-07-18 11:42:54.946Z	4.209° NNE	2025-07-18 11:49:54.946Z	286.19° WNW	38.594°	2025-07-18 11:56:54.946Z	222.841° SW
13 mins	2025-07-18 20:46:54.946Z	124.819° SE	2025-07-18 20:52:54.946Z	67.201° ENE	33.305°	2025-07-18 20:59:54.946Z	358.938° N
13 mins	2025-07-18 22:39:54.946Z	197.581° SSW	2025-07-18 22:45:54.946Z	266.476° W	34.565°	2025-07-18 22:52:54.946Z	329.828° NNW

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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Authenticating...

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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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