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: 19 hours ago
TLE from 19 hours ago
0 EZIE-C
1 63249U 25052AR 26206.53071211 .00003775 00000-0 32832-3 0 9997
2 63249 97.6845 97.9594 0005216 83.2142 276.9674 14.97552991 74400Epoch: 2026-07-25T12:44Z
TLE epoch observation values (Epoch: 2026-07-25T12:44:13.526Z)
Latitude
0.00003°
Longitude
-36.33863°
Altitude
577.073 km
Speed
7.572 km/s
True Right ascension
06h 31m 50s
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
21:09:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.093 km
Perigee altitude
567.843 km
Semi-major axis
6,949.605 km
Eccentricity
0.00052
Inclination
97.6845°
RAAN
97.9594°
Arg. of periapsis
83.2142°
True anomaly
276.90807°
Mean anomaly
276.9674°
Eccentric anomaly
276.93773°
Mean motion
3.7463 °/min
Orbital period
96.09 mins
BSTAR
0.00032832
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-26 16:08:16.781Z | 125.432° SE | 2026-07-26 16:11:16.781Z | 69.654° E | 25.166° | 2026-07-26 16:14:16.781Z | 14.76° NNE |
| 4 mins | 2026-07-26 17:45:16.781Z | 241.552° WSW | 2026-07-26 17:46:16.781Z | 261.71° W | 19.541° | 2026-07-26 17:49:16.781Z | 312.765° NW |
| 6 mins | 2026-07-27 05:24:16.781Z | 27.404° NE | 2026-07-27 05:27:16.781Z | 112.509° SE | 38.504° | 2026-07-27 05:30:16.781Z | 174.848° S |
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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