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: 10 hours ago
TLE from 10 hours ago
0 TOMORROW-S3
1 62392U 24247R 25300.83494264 .00014280 00000-0 57340-3 0 9998
2 62392 44.9946 120.7868 0002892 212.6856 147.3847 15.24920686 47438Epoch: 2025-10-27T20:02Z
TLE epoch observation values (Epoch: 2025-10-27T20:02:19.044Z)
Latitude
-0.00002°
Longitude
143.77634°
Altitude
492.695 km
Speed
7.619 km/s
True Right ascension
08h 03m 08s
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
01:33:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.619 km
Perigee altitude
490.645 km
Semi-major axis
6,870.769 km
Eccentricity
0.00029
Inclination
44.9946°
RAAN
120.7868°
Arg. of periapsis
212.6856°
True anomaly
147.40256°
Mean anomaly
147.3847°
Eccentric anomaly
147.39363°
Mean motion
3.81097 °/min
Orbital period
94.46 mins
BSTAR
0.0005734
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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 | 2025-10-28 15:05:57.441Z | 212.792° SW | 2025-10-28 15:08:57.441Z | 144.432° SSE | 32.185° | 2025-10-28 15:11:57.441Z | 80.543° E |
| 5 mins | 2025-10-28 16:45:57.441Z | 276.618° WNW | 2025-10-28 16:47:57.441Z | 354.4° N | 38.943° | 2025-10-28 16:50:57.441Z | 60.421° ENE |
| 5 mins | 2025-10-28 18:24:57.441Z | 303.943° NW | 2025-10-28 18:26:57.441Z | 352.616° N | 30.924° | 2025-10-28 18:29:57.441Z | 66.244° ENE |
| 6 mins | 2025-10-28 20:03:57.441Z | 298.558° NW | 2025-10-28 20:06:57.441Z | 71.357° E | 41.56° | 2025-10-28 20:09:57.441Z | 105.36° ESE |
| 4 mins | 2025-10-28 21:43:57.441Z | 248.6° W | 2025-10-28 21:44:57.441Z | 224.645° SW | 22.978° | 2025-10-28 21:47:57.441Z | 164.202° 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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