EZIE-B, 63250
Orbit data source: Space-Track
EZIE-B, 63250 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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63250 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-B
1 63250U 25052AS 26171.44353431 .00003182 00000-0 27962-3 0 9997
2 63250 97.6897 63.6157 0004110 151.4006 208.7442 14.97256097 69153Epoch: 2026-06-20T10:38Z
TLE epoch observation values (Epoch: 2026-06-20T10:38:41.364Z)
Latitude
-0.00002°
Longitude
-4.71473°
Altitude
580.937 km
Speed
7.569 km/s
True Right ascension
04h 14m 27s
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
07:24:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.244 km
Perigee altitude
569.531 km
Semi-major axis
6,950.524 km
Eccentricity
0.00041
Inclination
97.6897°
RAAN
63.6157°
Arg. of periapsis
151.4006°
True anomaly
208.72156°
Mean anomaly
208.7442°
Eccentric anomaly
208.73288°
Mean motion
3.74556 °/min
Orbital period
96.11 mins
BSTAR
0.00027962
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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-B 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 | 2026-06-21 04:52:42.897Z | 53.064° ENE | 2026-06-21 04:54:42.897Z | 88.911° E | 20.287° | 2026-06-21 04:57:42.897Z | 142.143° SSE |
| 4 mins | 2026-06-21 06:28:42.897Z | 324.035° NNW | 2026-06-21 06:29:42.897Z | 301.993° NW | 23.841° | 2026-06-21 06:32:42.897Z | 240.368° WSW |
| 5 mins | 2026-06-21 17:15:42.897Z | 200.975° SSW | 2026-06-21 17:17:42.897Z | 261.774° W | 35.748° | 2026-06-21 17:20:42.897Z | 330.296° NNW |
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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