MINOTAUR 4 DEB, 54256
Orbit data source: Space-Track
MINOTAUR 4 DEB, 54256 is space debris in LEO originally from a launch on Wed, 15 Jul 2020 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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54256 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NGIS FSG
Mission
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: 22 hours ago
TLE from 22 hours ago
0 MINOTAUR 4 DEB
1 54256U 20046AK 25350.26374589 .00017373 00000-0 68743-3 0 9995
2 54256 54.2395 345.0853 0020119 70.3761 289.9420 15.25407907218271Epoch: 2025-12-16T06:19Z
TLE epoch observation values (Epoch: 2025-12-16T06:19:47.644Z)
Latitude
-0.00012°
Longitude
164.98624°
Altitude
485.886 km
Speed
7.626 km/s
True Right ascension
23h 00m 20s
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
02:43:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.461 km
Perigee altitude
475.827 km
Semi-major axis
6,867.781 km
Eccentricity
0.00201
Inclination
54.2395°
RAAN
345.0853°
Arg. of periapsis
70.3761°
True anomaly
289.72509°
Mean anomaly
289.942°
Eccentric anomaly
289.83356°
Mean motion
3.81345 °/min
Orbital period
94.4 mins
BSTAR
0.00068743
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Other satellites on launch #46 in the year 2020 (2020-07-15 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.MINOTAUR 4 DEB 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-17 07:57:39.288Z | 356.583° N | 2025-12-17 07:58:39.288Z | 16.694° NNE | 17.972° | 2025-12-17 08:01:39.288Z | 72.284° E |
| 5 mins | 2025-12-17 09:35:39.288Z | 303.361° NW | 2025-12-17 09:37:39.288Z | 203.798° SW | 43.452° | 2025-12-17 09:40:39.288Z | 140.714° SSE |
| 5 mins | 2025-12-18 02:34:39.288Z | 260.315° W | 2025-12-18 02:36:39.288Z | 338.578° N | 36.384° | 2025-12-18 02:39:39.288Z | 37.511° NE |
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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