SCOUT X-1 DEB, 3927 (Decayed)
Orbit data source: Space-Track
SCOUT X-1 DEB, 3927 was space debris in LEO originally from a launch on Thu, 16 Feb 1961 UTC launched from the Wallops Island (WLPIS). 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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3927 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 SCOUT X-1 DEB
1 03927U 61004F 26076.61522767 .03359307 11842-1 10780-1 0 9993
2 03927 39.0176 168.8208 0011511 35.2297 324.9271 15.92787666117115Epoch: 2026-03-17T14:45Z
TLE epoch observation values (Epoch: 2026-03-17T14:45:55.670Z)
Latitude
0.00002°
Longitude
132.14805°
Altitude
287.521 km
Speed
7.741 km/s
True Right ascension
11h 15m 16s
True Declination
0° 00' 00"
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
06:56:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
304.851 km
Perigee altitude
289.483 km
Semi-major axis
6,675.304 km
Eccentricity
0.00115
Inclination
39.0176°
RAAN
168.8208°
Arg. of periapsis
35.2297°
True anomaly
324.85121°
Mean anomaly
324.9271°
Eccentric anomaly
324.88917°
Mean motion
3.97957 °/min
Orbital period
90.46 mins
BSTAR
0.01078
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Other satellites on launch #4 in the year 1961 (1961-02-16 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 X-1 DEB Visibility
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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. |
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| This satellite is decayed. |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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