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, 0.5 m
Radar Cross Section
0.625 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 SPHEREX
1 63182U 25047E 25257.51813657 .00000960 00000-0 15648-3 0 9997
2 63182 97.9572 82.6123 0010653 4.4330 355.6971 14.73150667 27445Epoch: 2025-09-14T12:26Z
TLE epoch observation values (Epoch: 2025-09-14T12:26:06.999Z)
Latitude
0.00002°
Longitude
-97.65286°
Altitude
646.57 km
Speed
7.539 km/s
True Right ascension
05h 30m 26s
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
23:28:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.565 km
Perigee altitude
640.595 km
Semi-major axis
7,026.217 km
Eccentricity
0.00107
Inclination
97.9572°
RAAN
82.6123°
Arg. of periapsis
4.433°
True anomaly
355.68793°
Mean anomaly
355.6971°
Eccentric anomaly
355.69252°
Mean motion
3.6852 °/min
Orbital period
97.69 mins
BSTAR
0.00015648
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-15 11:24:50.999Z | 106.219° ESE | 2025-09-15 11:27:50.999Z | 57.515° ENE | 18.633° | 2025-09-15 11:29:50.999Z | 27.281° NE |
| 7 mins | 2025-09-15 13:00:50.999Z | 202.157° SSW | 2025-09-15 13:03:50.999Z | 262.786° W | 30.811° | 2025-09-15 13:07:50.999Z | 329.49° NNW |
| 7 mins | 2025-09-16 00:52:50.999Z | 31.385° NE | 2025-09-16 00:55:50.999Z | 90.544° ESE | 35.284° | 2025-09-16 00:59:50.999Z | 170.197° S |
| 4 mins | 2025-09-16 02:30:50.999Z | 319.293° NNW | 2025-09-16 02:32:50.999Z | 287.445° WNW | 16.23° | 2025-09-16 02:34:50.999Z | 259.217° W |
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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