SPHEREX, 63182
Orbit data source: Space-Track
SPHEREX, 63182 is an American payload satellite 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SWRI
Mission
Operational Civil Astronomy
Bus & Motor
PUNCH, Unknown motor
Mass
64 kg wet, 64 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: 5 hours ago
TLE from 5 hours ago
0 SPHEREX
1 63182U 25047E 25291.27407253 .00002095 00000-0 33147-3 0 9994
2 63182 97.9554 115.7028 0009370 246.9614 113.0607 14.73299416 32410Epoch: 2025-10-18T06:34Z
TLE epoch observation values (Epoch: 2025-10-18T06:34:39.866Z)
Latitude
0.00003°
Longitude
-9.97076°
Altitude
656.151 km
Speed
7.528 km/s
True Right ascension
07h 42m 48s
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
06:37:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.19 km
Perigee altitude
641.024 km
Semi-major axis
7,025.744 km
Eccentricity
0.00094
Inclination
97.9554°
RAAN
115.7028°
Arg. of periapsis
246.9614°
True anomaly
113.15945°
Mean anomaly
113.0607°
Eccentric anomaly
113.11008°
Mean motion
3.68557 °/min
Orbital period
97.68 mins
BSTAR
0.00033147
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-18 13:13:15.998Z | 211.61° SW | 2025-10-18 13:16:15.998Z | 261.224° W | 24.348° | 2025-10-18 13:19:15.998Z | 314.358° NW |
| 7 mins | 2025-10-19 01:05:15.998Z | 22.261° NNE | 2025-10-19 01:08:15.998Z | 78.614° E | 41.515° | 2025-10-19 01:12:15.998Z | 181.422° SSW |
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 ascending 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 ascending order |
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