SPHEREX DEB, 63332

Orbit data source: Space-Track

SPHEREX DEB, 63332 is space debris in SSO originally from a launch on Wed, 12 Mar 2025 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
63332, 2025-047F
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
BAEB
Mission
Spacecraft
Bus & Motor
SPHEREX, Unknown motor
Mass
~5 kg wet, ~5 kg dry
Launch date (UTC)
2025-03-12 (1 year ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.2 m
Radar Cross Section
0.188 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 SPHEREX DEB
1 63332U 25047F   26077.46853182  .00006005  00000-0  80434-3 0  9997
2 63332  97.9523 265.6535 0008041 107.2555 252.9537 14.79764381 53690
Epoch: 2026-03-18T11:14Z
TLE epoch observation values (Epoch: 2026-03-18T11:14:41.149Z)
Latitude
-0.00003°
Longitude
-79.04982°
Altitude
634.744 km
Speed
7.54 km/s
True Right ascension
17h 42m 36s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
10:00:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.744 km
Perigee altitude
621.479 km
Semi-major axis
7,005.248 km
Eccentricity
0.0008
Inclination
97.9523°
RAAN
265.6535°
Arg. of periapsis
107.2555°
True anomaly
252.86563°
Mean anomaly
252.9537°
Eccentric anomaly
252.90966°
Mean motion
3.70176 °/min
Orbital period
97.25 mins
BSTAR
0.00080434
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Other satellites on launch #47 in the year 2025 (2025-03-12 UTC)

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