SPHEREX, 63182
Orbit data source: Space-Track
SPHEREX, 63182 is a payload satellite owned by JPL (US) in SSO that was launched on Wed, 12 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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63182 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
BAEB
Mission
Operational Civil Astronomy
Bus & Motor
SPHEREX, Unknown motor
Mass
502 kg wet, 502 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 2.7 m
Radar Cross Section
0.625 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SPHEREX
1 63182U 25047E 26305.22684493 .00000716 00000-0 11564-3 0 9996
2 63182 97.9578 127.5801 0011514 110.7371 249.5073 14.74282311 88237Epoch: 2026-11-01T05:26Z
TLE epoch observation values (Epoch: 2026-11-01T05:26:39.401Z)
Latitude
-0.00002°
Longitude
5.39468°
Altitude
653.283 km
Speed
7.529 km/s
True Right ascension
08h 30m 19s
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
13:43:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.567 km
Perigee altitude
636.396 km
Semi-major axis
7,022.618 km
Eccentricity
0.00115
Inclination
97.9578°
RAAN
127.5801°
Arg. of periapsis
110.7371°
True anomaly
249.38377°
Mean anomaly
249.5073°
Eccentric anomaly
249.44553°
Mean motion
3.68803 °/min
Orbital period
97.61 mins
BSTAR
0.00011564
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Other satellites on launch #47 in the year 2025 (2025-03-12 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.SPHEREX 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-02 01:33:46.245Z | 357.937° N | 2026-11-02 01:36:46.245Z | 299.277° NW | 50.957° | 2026-11-02 01:40:46.245Z | 213.077° SW |
| 7 mins | 2026-11-02 12:31:46.245Z | 181.843° SSW | 2026-11-02 12:34:46.245Z | 291.445° WNW | 61.908° | 2026-11-02 12:38:46.245Z | 341.509° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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