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: 11 hours ago
TLE from 11 hours ago
0 TOMORROW-S3
1 62392U 24247R 25346.93628569 .00009882 00000-0 38815-3 0 9994
2 62392 45.0056 229.9351 0001378 121.4740 238.6277 15.25976794 54473Epoch: 2025-12-12T22:28Z
TLE epoch observation values (Epoch: 2025-12-12T22:28:15.083Z)
Latitude
-0.00005°
Longitude
171.00145°
Altitude
488.346 km
Speed
7.622 km/s
True Right ascension
15h 19m 44s
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
07:35:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.407 km
Perigee altitude
488.515 km
Semi-major axis
6,867.598 km
Eccentricity
0.00014
Inclination
45.0056°
RAAN
229.9351°
Arg. of periapsis
121.474°
True anomaly
238.61422°
Mean anomaly
238.6277°
Eccentric anomaly
238.62096°
Mean motion
3.81361 °/min
Orbital period
94.4 mins
BSTAR
0.00038815
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-13 19:05:18.225Z | 199.249° SSW | 2025-12-13 19:07:18.225Z | 157.891° S | 26.487° | 2025-12-13 19:10:18.225Z | 88.36° E |
| 5 mins | 2025-12-13 20:44:18.225Z | 265.907° W | 2025-12-13 20:46:18.225Z | 327.695° NNW | 41.374° | 2025-12-13 20:49:18.225Z | 60.492° ENE |
| 5 mins | 2025-12-13 22:23:18.225Z | 299.554° NW | 2025-12-13 22:25:18.225Z | 343.36° N | 30.048° | 2025-12-13 22:28:18.225Z | 61.67° ENE |
| 6 mins | 2025-12-14 00:02:18.225Z | 300.585° NW | 2025-12-14 00:05:18.225Z | 44.232° NE | 40.287° | 2025-12-14 00:08:18.225Z | 98.359° ESE |
| 4 mins | 2025-12-14 01:42:18.225Z | 256.297° W | 2025-12-14 01:43:18.225Z | 230.313° WSW | 27.141° | 2025-12-14 01:46:18.225Z | 157.611° 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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