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: 19 hours ago
TLE from 19 hours ago
0 SPHEREX
1 63182U 25047E 25258.53697541 .00001071 00000-0 17375-3 0 9995
2 63182 97.9572 83.6110 0010565 1.2017 358.9214 14.73153523 27597Epoch: 2025-09-15T12:53Z
TLE epoch observation values (Epoch: 2025-09-15T12:53:14.675Z)
Latitude
-0.00008°
Longitude
-104.44035°
Altitude
646.603 km
Speed
7.538 km/s
True Right ascension
05h 34m 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
00:05:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.495 km
Perigee altitude
640.648 km
Semi-major axis
7,026.208 km
Eccentricity
0.00106
Inclination
97.9572°
RAAN
83.611°
Arg. of periapsis
1.2017°
True anomaly
358.91912°
Mean anomaly
358.9214°
Eccentric anomaly
358.92026°
Mean motion
3.6852 °/min
Orbital period
97.69 mins
BSTAR
0.00017375
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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 | 2025-09-16 11:50:28.926Z | 134.383° SE | 2025-09-16 11:54:28.926Z | 55.328° ENE | 30.199° | 2025-09-16 11:57:28.926Z | 7.859° NNE |
| 4 mins | 2025-09-16 13:29:28.926Z | 243.311° WSW | 2025-09-16 13:30:28.926Z | 260.361° W | 18.052° | 2025-09-16 13:33:28.926Z | 307.233° NW |
| 7 mins | 2025-09-17 01:19:28.926Z | 12.579° NNE | 2025-09-17 01:22:28.926Z | 11.976° NNE | 43.791° | 2025-09-17 01:26:28.926Z | 194.004° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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