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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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 SPHEREX
1 63182U 25047E 26035.46615940 .00001631 00000-0 25722-3 0 9991
2 63182 97.9545 222.7631 0009263 257.8767 102.1404 14.73734829 48491Epoch: 2026-02-04T11:11Z
TLE epoch observation values (Epoch: 2026-02-04T11:11:16.172Z)
Latitude
0.00002°
Longitude
-79.68662°
Altitude
653.557 km
Speed
7.53 km/s
True Right ascension
14h 51m 03s
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
20:15:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.729 km
Perigee altitude
639.715 km
Semi-major axis
7,024.359 km
Eccentricity
0.00093
Inclination
97.9545°
RAAN
222.7631°
Arg. of periapsis
257.8767°
True anomaly
102.24415°
Mean anomaly
102.1404°
Eccentric anomaly
102.19228°
Mean motion
3.68666 °/min
Orbital period
97.65 mins
BSTAR
0.00025722
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Other satellites on launch #47 in the year 2025 (2025-03-12 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-05 00:47:31.354Z | 26.978° NE | 2026-02-05 00:51:31.354Z | 93.752° ESE | 34.502° | 2026-02-05 00:55:31.354Z | 169.425° S |
| 4 mins | 2026-02-05 02:26:31.354Z | 318.164° NNW | 2026-02-05 02:27:31.354Z | 302.439° NW | 16.592° | 2026-02-05 02:30:31.354Z | 257.35° W |
| 6 mins | 2026-02-05 11:46:31.354Z | 127.133° SE | 2026-02-05 11:49:31.354Z | 63.992° ENE | 30.105° | 2026-02-05 11:52:31.354Z | 10.693° NNE |
| 4 mins | 2026-02-05 13:24:31.354Z | 239.188° WSW | 2026-02-05 13:26:31.354Z | 274.632° WNW | 18.892° | 2026-02-05 13:28:31.354Z | 305.309° NW |
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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