OBJECT A, 67219
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT A, 67219 is a satellite owned by USAF STP (US) in LEO that was launched on Thu, 18 Dec 2025 UTC via an ELECTRON launch vehicle from the Wallops Island (WLPIS). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
AERO
Mission
Operational spacecraft
Bus & Motor
DISKSAT, EP
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OBJECT A
1 67219U 25305A 25354.38090451 .00000510 00000-0 50887-4 0 9997
2 67219 45.0057 310.0654 0003912 276.1097 83.9332 15.05762698 337Epoch: 2025-12-20T09:08Z
TLE epoch observation values (Epoch: 2025-12-20T09:08:30.149Z)
Latitude
-0.00002°
Longitude
83.73123°
Altitude
548.879 km
Speed
7.589 km/s
True Right ascension
20h 40m 15s
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
12:16:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
553.469 km
Perigee altitude
548.048 km
Semi-major axis
6,928.895 km
Eccentricity
0.00039
Inclination
45.0057°
RAAN
310.0654°
Arg. of periapsis
276.1097°
True anomaly
83.97778°
Mean anomaly
83.9332°
Eccentric anomaly
83.95549°
Mean motion
3.76311 °/min
Orbital period
95.67 mins
BSTAR
0.000050887
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Other satellites on launch #305 in the year 2025 (2025-12-18 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.OBJECT A 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-21 23:32:33.364Z | 198.868° SSW | 2025-12-21 23:35:33.364Z | 135.329° SSE | 27.053° | 2025-12-21 23:38:33.364Z | 84.175° E |
| 6 mins | 2025-12-22 01:12:33.364Z | 260.308° W | 2025-12-22 01:15:33.364Z | 1.074° NNE | 42.512° | 2025-12-22 01:18:33.364Z | 62.037° ENE |
| 6 mins | 2025-12-22 02:53:33.364Z | 298.675° NW | 2025-12-22 02:55:33.364Z | 340.625° N | 31.839° | 2025-12-22 02:59:33.364Z | 67.929° E |
| 6 mins | 2025-12-22 04:34:33.364Z | 304.171° NW | 2025-12-22 04:36:33.364Z | 2.348° NNE | 41.359° | 2025-12-22 04:40:33.364Z | 99.152° ESE |
| 6 mins | 2025-12-22 06:14:33.364Z | 269.272° W | 2025-12-22 06:16:33.364Z | 226.335° WSW | 29.646° | 2025-12-22 06:20:33.364Z | 149.217° SSE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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