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: 12 hours ago
TLE from 12 hours ago
0 TOMORROW-S3
1 62392U 24247R 26219.76957237 .00003736 00000-0 13768-3 0 9994
2 62392 45.0010 10.7365 0003775 262.5836 97.4619 15.29706633 90850Epoch: 2026-08-07T18:28Z
TLE epoch observation values (Epoch: 2026-08-07T18:28:11.052Z)
Latitude
-0.00003°
Longitude
137.39991°
Altitude
477.024 km
Speed
7.629 km/s
True Right ascension
00h 42m 56s
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
20:48:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.887 km
Perigee altitude
475.711 km
Semi-major axis
6,856.436 km
Eccentricity
0.00038
Inclination
45.001°
RAAN
10.7365°
Arg. of periapsis
262.5836°
True anomaly
97.50479°
Mean anomaly
97.4619°
Eccentric anomaly
97.48334°
Mean motion
3.82292 °/min
Orbital period
94.17 mins
BSTAR
0.00013768
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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 | 2026-08-08 13:29:02.681Z | 227.416° WSW | 2026-08-08 13:32:02.681Z | 159.873° S | 39.636° | 2026-08-08 13:35:02.681Z | 74.948° E |
| 5 mins | 2026-08-08 15:09:02.681Z | 287.604° WNW | 2026-08-08 15:11:02.681Z | 355.945° N | 34.982° | 2026-08-08 15:14:02.681Z | 59.949° ENE |
| 5 mins | 2026-08-08 16:48:02.681Z | 310.069° NW | 2026-08-08 16:50:02.681Z | 8.755° NNE | 31.911° | 2026-08-08 16:53:02.681Z | 74.213° E |
| 5 mins | 2026-08-08 18:27:02.681Z | 292.494° WNW | 2026-08-08 18:29:02.681Z | 134.701° SE | 44.668° | 2026-08-08 18:32:02.681Z | 116.108° 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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