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: 12 hours ago
TLE from 12 hours ago
0 EZIE-B
1 63250U 25052AS 26264.92034084 .00003307 00000-0 28601-3 0 9993
2 63250 97.6768 155.5642 0002208 193.5700 166.5463 14.97857896 83147Epoch: 2026-09-21T22:05Z
TLE epoch observation values (Epoch: 2026-09-21T22:05:17.448Z)
Latitude
-0.00006°
Longitude
-176.55174°
Altitude
578.062 km
Speed
7.571 km/s
True Right ascension
10h 22m 15s
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
02:50:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.058 km
Perigee altitude
568.989 km
Semi-major axis
6,948.66 km
Eccentricity
0.00022
Inclination
97.6768°
RAAN
155.5642°
Arg. of periapsis
193.57°
True anomaly
166.55219°
Mean anomaly
166.5463°
Eccentric anomaly
166.54924°
Mean motion
3.74707 °/min
Orbital period
96.08 mins
BSTAR
0.00028601
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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 | 2026-09-22 15:52:44.529Z | 107.069° ESE | 2026-09-22 15:54:44.529Z | 74.676° E | 18.902° | 2026-09-22 15:57:44.529Z | 24.79° NE |
| 6 mins | 2026-09-22 17:27:44.529Z | 210.606° SW | 2026-09-22 17:29:44.529Z | 252.942° W | 31.845° | 2026-09-22 17:33:44.529Z | 327.404° NNW |
| 5 mins | 2026-09-23 05:08:44.529Z | 49.365° ENE | 2026-09-23 05:10:44.529Z | 100.134° ESE | 33.582° | 2026-09-23 05:13:44.529Z | 158.643° 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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