SCOUT X-4 R/B, 809

Orbit data source: Space-Track

SCOUT X-4 R/B, 809 is space debris in LEO originally from a launch on Thu, 04 Jun 1964 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/809?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/809?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

809, 1964-026D

Orbit

LEO

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)

1964-06-04 (61 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 22 hours ago

0 SCOUT X-4 R/B
1 00809U 64026D   25128.94982023  .00000439  00000-0  24016-3 0  9992
2 00809  90.4512 157.5336 0037385 277.1544  82.5391 14.10541706121153

Epoch: 2025-05-08T22:47Z

Definitive object data (Epoch: 2025-05-08T22:47:44.467Z)

Latitude

-0.00004°

Longitude

-51.41465°

Altitude

857.146 km

Speed

7.426 km/s

True Right ascension

10h 30m 08s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-24.49017°

Longitude

-51.16398°

Altitude

853.803 km

Speed

7.431 km/s

Apparent Right ascension

13h 07m 44s

Apparent Declination

-42° 29' 52"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

05:00:01

Azimuth

113.179° SE

Elevation

-47.103°

Doppler factor

Orbital elements

Apogee altitude

881.52 km

Perigee altitude

827.442 km

Semi-major axis

7,232.618 km

Eccentricity

0.0037385

Inclination

90.4512°

RAAN

157.5336°

Arg. of periapsis

277.1544°

True anomaly

82.96413°

Mean anomaly

82.5391°

Eccentric anomaly

82.75159°

Mean motion

3.52858 °/min

BSTAR

0.00024016

Orbital period

102.02 mins

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Other satellites on launch #26 in the year 1964 (1964-06-04 UTC)

OPS 4412 (TRANSIT 9), 801

SCOUT X-4 DEB, 805

SCOUT X-4 DEB, 806 (Decayed)

SCOUT X-4 DEB, 2986

TRANSIT 9 DEB, 12142 (Decayed)

TRANSIT 9 DEB, 13360 (Decayed)

TRANSIT 9 DEB, 24272 (Decayed)

TRANSIT 9 DEB, 25056 (Decayed)

SCOUT X-4 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.
9 mins	2025-05-10 02:09:49.593Z	172.51° S	2025-05-10 02:13:49.593Z	25.498° NE	44.528°	2025-05-10 02:18:49.593Z	358.571° N
5 mins	2025-05-10 12:52:49.593Z	56.302° ENE	2025-05-10 12:54:49.593Z	80.696° E	16.141°	2025-05-10 12:57:49.593Z	114.916° SE
9 mins	2025-05-10 14:32:49.593Z	352.541° N	2025-05-10 14:36:49.593Z	290.662° WNW	41.12°	2025-05-10 14:41:49.593Z	199.57° SSW

Authenticating...

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Check out SCOUT X-4 R/B, 809 on other resources

View SCOUT X-4 R/B, 809 on Heavens-Above

View SCOUT X-4 R/B, 809 on Keep Track

View SCOUT X-4 R/B, 809 on Celestrak

View SCOUT X-4 R/B, 809 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.