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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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 TOMORROW-S3
1 62392U 24247R 26036.71146377 .00014022 00000-0 52918-3 0 9991
2 62392 45.0003 291.4460 0000740 290.5709 69.5094 15.27004826 62843Epoch: 2026-02-05T17:04Z
TLE epoch observation values (Epoch: 2026-02-05T17:04:30.469Z)
Latitude
-0.00006°
Longitude
-100.54078°
Altitude
484.593 km
Speed
7.625 km/s
True Right ascension
19h 25m 47s
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
08:19:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.889 km
Perigee altitude
485.873 km
Semi-major axis
6,864.518 km
Eccentricity
0.00007
Inclination
45.0003°
RAAN
291.446°
Arg. of periapsis
290.5709°
True anomaly
69.51734°
Mean anomaly
69.5094°
Eccentric anomaly
69.51337°
Mean motion
3.81617 °/min
Orbital period
94.34 mins
BSTAR
0.00052918
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-06 19:57:39.989Z | 225.013° WSW | 2026-02-06 20:01:39.989Z | 121.941° SE | 36.031° | 2026-02-06 20:04:39.989Z | 74.349° E |
| 6 mins | 2026-02-06 21:37:39.989Z | 278.637° WNW | 2026-02-06 21:39:39.989Z | 324.726° NNW | 35.284° | 2026-02-06 21:43:39.989Z | 62.113° ENE |
| 5 mins | 2026-02-06 23:17:39.989Z | 313.851° NW | 2026-02-06 23:19:39.989Z | 19.045° NNE | 31.142° | 2026-02-06 23:22:39.989Z | 74.237° E |
| 5 mins | 2026-02-07 00:56:39.989Z | 295.664° NW | 2026-02-07 00:58:39.989Z | 94.451° ESE | 44.352° | 2026-02-07 01:01:39.989Z | 112.622° SE |
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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