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, 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 26094.06184572 .00013132 00000-0 47964-3 0 9998
2 62392 45.0046 338.3721 0002865 254.6323 105.4243 15.28136223 71613Epoch: 2026-04-04T01:29Z
TLE epoch observation values (Epoch: 2026-04-04T01:29:03.470Z)
Latitude
-0.00007°
Longitude
123.72055°
Altitude
481.906 km
Speed
7.626 km/s
True Right ascension
22h 33m 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
20:15:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.959 km
Perigee altitude
481.027 km
Semi-major axis
6,861.13 km
Eccentricity
0.00029
Inclination
45.0046°
RAAN
338.3721°
Arg. of periapsis
254.6323°
True anomaly
105.45595°
Mean anomaly
105.4243°
Eccentric anomaly
105.44012°
Mean motion
3.819 °/min
Orbital period
94.27 mins
BSTAR
0.00047964
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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 | 2026-04-04 18:55:30.950Z | 200.811° SSW | 2026-04-04 18:58:30.950Z | 137.858° SSE | 25.233° | 2026-04-04 19:01:30.950Z | 84.189° E |
| 6 mins | 2026-04-04 20:34:30.950Z | 261.945° W | 2026-04-04 20:36:30.950Z | 304.516° NW | 41.043° | 2026-04-04 20:40:30.950Z | 63.408° ENE |
| 4 mins | 2026-04-04 22:14:30.950Z | 312.24° NW | 2026-04-04 22:15:30.950Z | 340.058° N | 29.714° | 2026-04-04 22:18:30.950Z | 60.223° ENE |
| 6 mins | 2026-04-04 23:52:30.950Z | 301.561° NW | 2026-04-04 23:55:30.950Z | 45.362° ENE | 39.033° | 2026-04-04 23:58:30.950Z | 96.519° ESE |
| 5 mins | 2026-04-05 01:31:30.950Z | 270.569° WNW | 2026-04-05 01:33:30.950Z | 224.622° SW | 29.163° | 2026-04-05 01:36:30.950Z | 152.918° SSE |
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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