SCOUT A DEB, 2702

Orbit data source: Space-Track

SCOUT A DEB, 2702 is space debris in LEO originally from a launch on Thu, 18 Aug 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/2702?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/2702?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2702, 1966-076D

Orbit

LEO

Last TLE update

23 hours ago

Origin

United States Navy (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-08-18 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 23 hours ago

0 SCOUT A DEB
1  2702U 66076D   25198.32223995  .00000064  00000-0  97177-4 0  9991
2  2702  88.5728 305.3037 0089602 137.7973 280.4115 13.36483274852067

Epoch: 2025-07-17T07:44Z

TLE epoch observation values (Epoch: 2025-07-17T07:44:01.531Z)

Latitude

57.26151°

Longitude

-103.88293°

Altitude

1,120.523 km

Speed

7.303 km/s

True Right ascension

20h 30m 03s

True Declination

57° 06' 45"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

82.13577°

Longitude

-95.89214°

Altitude

1,095.022 km

Speed

7.332 km/s

Apparent Right ascension

07h 41m 22s

Apparent Declination

40° 09' 25"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

19:57:55

Azimuth

3.208° NNE

Elevation

-9.838°

Doppler factor

Orbital elements

Apogee altitude

1,186.663 km

Perigee altitude

1,052.303 km

Semi-major axis

7,497.62 km

Eccentricity

0.00896

Inclination

88.5728°

RAAN

305.3037°

Arg. of periapsis

137.7973°

True anomaly

279.39965°

Mean anomaly

280.4115°

Eccentric anomaly

279.90577°

Mean motion

3.34317 °/min

Orbital period

107.68 mins

BSTAR

0.000097177

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Other satellites on launch #76 in the year 1966 (1966-08-18 UTC)

OPS 2366 (TRANSIT 14), 2401

SCOUT A R/B, 2413

SCOUT A DEB, 2580

TRANSIT 14 DEB, 7558 (Decayed)

TRANSIT 14 DEB, 8000 (Decayed)

TRANSIT 14 DEB, 9401 (Decayed)

TRANSIT 14 DEB, 26817

TRANSIT 14 DEB, 29138 (Decayed)

SCOUT A DEB 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.
11 mins	2025-07-18 08:42:58.517Z	223.427° SW	2025-07-18 08:47:58.517Z	272.491° WNW	25.723°	2025-07-18 08:53:58.517Z	336.401° NNW
8 mins	2025-07-18 18:12:58.517Z	37.146° NE	2025-07-18 18:16:58.517Z	85.717° E	23.177°	2025-07-18 18:20:58.517Z	128.473° SE
10 mins	2025-07-18 19:59:58.517Z	342.983° N	2025-07-18 20:04:58.517Z	264.625° W	36.404°	2025-07-18 20:09:58.517Z	207.59° SW
9 mins	2025-07-19 06:17:58.517Z	123.601° SE	2025-07-19 06:21:58.517Z	82.745° E	23.673°	2025-07-19 06:26:58.517Z	28.853° NE

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 SCOUT A DEB, 2702 on other resources

View SCOUT A DEB, 2702 on Heavens-Above

View SCOUT A DEB, 2702 on Keep Track

View SCOUT A DEB, 2702 on Celestrak

View SCOUT A DEB, 2702 on Gunter's Space Page

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