OBJECT K, 63219
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 K, 63219 is a satellite in SSO that was launched on Sat, 15 Mar 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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63219 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.054 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT K
1 63219U 25052K 25269.26956990 .00024651 00000-0 10503-2 0 9994
2 63219 97.4124 161.6946 0003547 21.8313 338.3074 15.22944792 29778Epoch: 2025-09-26T06:28Z
TLE epoch observation values (Epoch: 2025-09-26T06:28:10.839Z)
Latitude
-0.00004°
Longitude
59.33068°
Altitude
497.792 km
Speed
7.617 km/s
True Right ascension
10h 46m 46s
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
10:18:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.363 km
Perigee altitude
491.488 km
Semi-major axis
6,872.063 km
Eccentricity
0.00035
Inclination
97.4124°
RAAN
161.6946°
Arg. of periapsis
21.8313°
True anomaly
338.29237°
Mean anomaly
338.3074°
Eccentric anomaly
338.29989°
Mean motion
3.80989 °/min
Orbital period
94.49 mins
BSTAR
0.0010503
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.OBJECT K 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-26 17:38:14.278Z | 211.735° SW | 2025-09-26 17:40:14.278Z | 250.33° W | 22.878° | 2025-09-26 17:43:14.278Z | 316.523° NNW |
| 4 mins | 2025-09-27 05:08:14.278Z | 59.082° ENE | 2025-09-27 05:10:14.278Z | 109.255° ESE | 22.216° | 2025-09-27 05:12:14.278Z | 147.093° SSE |
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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