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: 10 hours ago
TLE from 10 hours ago
0 SPHEREX
1 63182U 25047E 26171.44423838 .00000700 00000-0 11388-3 0 9992
2 63182 97.9578 356.2091 0010421 175.0871 185.0442 14.74069015 68522Epoch: 2026-06-20T10:39Z
TLE epoch observation values (Epoch: 2026-06-20T10:39:42.196Z)
Latitude
0.00004°
Longitude
-72.3755°
Altitude
658.415 km
Speed
7.524 km/s
True Right ascension
23h 44m 50s
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
07:19:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.478 km
Perigee altitude
637.841 km
Semi-major axis
7,023.296 km
Eccentricity
0.00104
Inclination
97.9578°
RAAN
356.2091°
Arg. of periapsis
175.0871°
True anomaly
185.03371°
Mean anomaly
185.0442°
Eccentric anomaly
185.03896°
Mean motion
3.6875 °/min
Orbital period
97.63 mins
BSTAR
0.00011388
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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 | 2026-06-21 00:16:44.290Z | 45.064° ENE | 2026-06-21 00:19:44.290Z | 88.443° E | 19.676° | 2026-06-21 00:22:44.290Z | 137.536° SSE |
| 5 mins | 2026-06-21 01:54:44.290Z | 335.333° NNW | 2026-06-21 01:56:44.290Z | 289.903° WNW | 28.698° | 2026-06-21 01:59:44.290Z | 232.856° WSW |
| 4 mins | 2026-06-21 11:16:44.290Z | 86.74° E | 2026-06-21 11:17:44.290Z | 70.031° E | 17.566° | 2026-06-21 11:20:44.290Z | 25.333° NE |
| 6 mins | 2026-06-21 12:51:44.290Z | 202.024° SSW | 2026-06-21 12:54:44.290Z | 276.524° WNW | 32.714° | 2026-06-21 12:57:44.290Z | 327.858° NNW |
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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