SCOUT A R/B, 2967
Orbit data source: Space-Track
SCOUT A R/B, 2967 is space debris in LEO originally from a launch on Mon, 25 Sep 1967 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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2967 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SCOUT A R/B
1 02967U 67092B 25299.79384243 .00000114 00000-0 15320-3 0 9995
2 02967 89.2545 26.7971 0048157 59.7455 60.4303 13.52355225863388Epoch: 2025-10-26T19:03Z
TLE epoch observation values (Epoch: 2025-10-26T19:03:07.985Z)
Latitude
59.4256°
Longitude
-115.64663°
Altitude
1,056.211 km
Speed
7.338 km/s
True Right ascension
13h 42m 09s
True Declination
59° 16' 51"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
00:55:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,096.476 km
Perigee altitude
1,024.831 km
Semi-major axis
7,438.79 km
Eccentricity
0.00482
Inclination
89.2545°
RAAN
26.7971°
Arg. of periapsis
59.7455°
True anomaly
60.91169°
Mean anomaly
60.4303°
Eccentric anomaly
60.67085°
Mean motion
3.3829 °/min
Orbital period
106.42 mins
BSTAR
0.0001532
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Other satellites on launch #92 in the year 1967 (1967-09-25 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SCOUT A R/B Visibility forecast
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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 | 2025-10-27 06:59:26.304Z | 202.956° SW | 2025-10-27 07:05:26.304Z | 278.255° WNW | 35.335° | 2025-10-27 07:10:26.304Z | 342.596° N |
| 12 mins | 2025-10-27 18:08:26.304Z | 3.525° NNE | 2025-10-27 18:14:26.304Z | 148.989° SSE | 44.187° | 2025-10-27 18:20:26.304Z | 179.668° S |
| 5 mins | 2025-10-27 19:57:26.304Z | 308.895° NW | 2025-10-27 19:59:26.304Z | 288.921° WNW | 14.529° | 2025-10-27 20:02:26.304Z | 260.266° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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