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: 17 hours ago
TLE from 17 hours ago
0 TOMORROW-S3
1 62392U 24247R 26282.70834889 .00006123 00000-0 21445-3 0 9999
2 62392 45.0009 25.8661 0003977 275.9816 84.0615 15.30381998100499Epoch: 2026-10-09T17:00Z
TLE epoch observation values (Epoch: 2026-10-09T17:00:01.344Z)
Latitude
0.00001°
Longitude
112.53456°
Altitude
474.39 km
Speed
7.631 km/s
True Right ascension
01h 43m 27s
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
03:54:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.009 km
Perigee altitude
473.557 km
Semi-major axis
6,854.42 km
Eccentricity
0.0004
Inclination
45.0009°
RAAN
25.8661°
Arg. of periapsis
275.9816°
True anomaly
84.10683°
Mean anomaly
84.0615°
Eccentric anomaly
84.08417°
Mean motion
3.82461 °/min
Orbital period
94.13 mins
BSTAR
0.00021445
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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 | 2026-10-10 10:26:45.090Z | 228.933° WSW | 2026-10-10 10:29:45.090Z | 140.419° SSE | 60.069° | 2026-10-10 10:32:45.090Z | 72.69° E |
| 5 mins | 2026-10-10 12:06:45.090Z | 293.478° NW | 2026-10-10 12:08:45.090Z | 8.259° NNE | 41.445° | 2026-10-10 12:11:45.090Z | 61.064° ENE |
| 5 mins | 2026-10-10 13:45:45.090Z | 315.194° NNW | 2026-10-10 13:47:45.090Z | 21.694° NNE | 37.699° | 2026-10-10 13:50:45.090Z | 76.69° E |
| 6 mins | 2026-10-10 15:23:45.090Z | 292.331° WNW | 2026-10-10 15:25:45.090Z | 283.166° WNW | 64.914° | 2026-10-10 15:29:45.090Z | 117.365° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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