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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Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Operational Civil Science
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
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: 10 hours ago
TLE from 10 hours ago
0 EZIE-C
1 63249U 25052AR 26144.98331650 .00004167 00000-0 36623-3 0 9991
2 63249 97.6906 37.4175 0001484 331.0339 29.0800 14.97089281 65198Epoch: 2026-05-24T23:35Z
TLE epoch observation values (Epoch: 2026-05-24T23:35:58.545Z)
Latitude
-0.00006°
Longitude
160.84593°
Altitude
578.044 km
Speed
7.572 km/s
True Right ascension
02h 29m 40s
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
18:24:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.936 km
Perigee altitude
571.873 km
Semi-major axis
6,951.041 km
Eccentricity
0.00015
Inclination
97.6906°
RAAN
37.4175°
Arg. of periapsis
331.0339°
True anomaly
29.08827°
Mean anomaly
29.08°
Eccentric anomaly
29.08413°
Mean motion
3.74514 °/min
Orbital period
96.12 mins
BSTAR
0.00036623
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-25 15:47:37.968Z | 106.466° ESE | 2026-05-25 15:50:37.968Z | 58.805° ENE | 15.945° | 2026-05-25 15:52:37.968Z | 28.487° NE |
| 6 mins | 2026-05-25 17:22:37.968Z | 203.448° SW | 2026-05-25 17:25:37.968Z | 279.23° WNW | 30.112° | 2026-05-25 17:28:37.968Z | 328.652° NNW |
| 5 mins | 2026-05-26 05:03:37.968Z | 45.624° ENE | 2026-05-26 05:05:37.968Z | 84.634° E | 25.76° | 2026-05-26 05:08:37.968Z | 149.436° SSE |
| 4 mins | 2026-05-26 06:39:37.968Z | 320.533° NNW | 2026-05-26 06:40:37.968Z | 301.881° NW | 19.023° | 2026-05-26 06:43:37.968Z | 248.857° W |
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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