EZIE-C, 63249
Orbit data source: Space-Track
EZIE-C, 63249 is an American payload 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). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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63249 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational Civil Science
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 EZIE-C
1 63249U 25052AR 25299.93922694 .00007423 00000-0 69640-3 0 9993
2 63249 97.7078 190.8910 0001890 291.1342 68.9676 14.94274651 33799Epoch: 2025-10-26T22:32Z
TLE epoch observation values (Epoch: 2025-10-26T22:32:29.207Z)
Latitude
-0.00005°
Longitude
177.22108°
Altitude
587.2 km
Speed
7.567 km/s
True Right ascension
12h 43m 33s
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
23:18:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.954 km
Perigee altitude
580.323 km
Semi-major axis
6,959.775 km
Eccentricity
0.00019
Inclination
97.7078°
RAAN
190.891°
Arg. of periapsis
291.1342°
True anomaly
68.98782°
Mean anomaly
68.9676°
Eccentric anomaly
68.97771°
Mean motion
3.7381 °/min
Orbital period
96.31 mins
BSTAR
0.0006964
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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.EZIE-C 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-27 05:31:42.645Z | 18.787° NNE | 2025-10-27 05:35:42.645Z | 101.47° ESE | 42.049° | 2025-10-27 05:39:42.645Z | 183.166° SSW |
| 6 mins | 2025-10-27 16:21:42.645Z | 131.76° SE | 2025-10-27 16:24:42.645Z | 60.525° ENE | 30.967° | 2025-10-27 16:27:42.645Z | 7.34° NNE |
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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