TOMORROW-S3, 62392
Orbit data source: Space-Track
TOMORROW-S3, 62392 is a payload satellite owned by Tomorrow.io (US) in LEO that was launched on Sat, 21 Dec 2024 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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62392 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Canyon
Mission
Operational Commercial Weather
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.138 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 TOMORROW-S3
1 62392U 24247R 26220.74911875 .00003789 00000-0 13945-3 0 9997
2 62392 45.0012 5.3719 0003813 266.1173 93.9275 15.29713831 91007Epoch: 2026-08-08T17:58Z
TLE epoch observation values (Epoch: 2026-08-08T17:58:43.859Z)
Latitude
-0.00004°
Longitude
138.43311°
Altitude
476.846 km
Speed
7.629 km/s
True Right ascension
00h 21m 29s
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
21:52:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.892 km
Perigee altitude
475.663 km
Semi-major axis
6,856.415 km
Eccentricity
0.00038
Inclination
45.0012°
RAAN
5.3719°
Arg. of periapsis
266.1173°
True anomaly
93.97109°
Mean anomaly
93.9275°
Eccentric anomaly
93.9493°
Mean motion
3.82294 °/min
Orbital period
94.17 mins
BSTAR
0.00013945
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Other satellites on launch #247 in the year 2024 (2024-12-21 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.TOMORROW-S3 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 | 2026-08-10 12:29:37.037Z | 222.979° SW | 2026-08-10 12:32:37.037Z | 163.721° S | 36.495° | 2026-08-10 12:35:37.037Z | 78.243° E |
| 5 mins | 2026-08-10 14:09:37.037Z | 282.833° WNW | 2026-08-10 14:11:37.037Z | 351.046° N | 36.388° | 2026-08-10 14:14:37.037Z | 59.558° ENE |
| 5 mins | 2026-08-10 15:48:37.037Z | 308.527° NW | 2026-08-10 15:50:37.037Z | 4.553° NNE | 31.333° | 2026-08-10 15:53:37.037Z | 71.454° E |
| 5 mins | 2026-08-10 17:27:37.037Z | 296.268° NW | 2026-08-10 17:29:37.037Z | 49.413° ENE | 44.792° | 2026-08-10 17:32:37.037Z | 111.417° ESE |
| 4 mins | 2026-08-10 19:06:37.037Z | 245.815° WSW | 2026-08-10 19:07:37.037Z | 224.766° SW | 18.743° | 2026-08-10 19:10:37.037Z | 170.645° S |
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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