TOMORROW-S4, 62386
Orbit data source: Space-Track
TOMORROW-S4, 62386 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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62386 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: 18 hours ago
TLE from 18 hours ago
0 TOMORROW-S4
1 62386U 24247K 26282.67146374 .00005952 00000-0 20834-3 0 9993
2 62386 44.9835 25.7935 0005179 317.9295 42.1191 15.30445152100480Epoch: 2026-10-09T16:06Z
TLE epoch observation values (Epoch: 2026-10-09T16:06:54.467Z)
Latitude
0.00001°
Longitude
125.77697°
Altitude
471.849 km
Speed
7.633 km/s
True Right ascension
01h 43m 10s
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
03:54:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.647 km
Perigee altitude
472.547 km
Semi-major axis
6,854.234 km
Eccentricity
0.00052
Inclination
44.9835°
RAAN
25.7935°
Arg. of periapsis
317.9295°
True anomaly
42.15892°
Mean anomaly
42.1191°
Eccentric anomaly
42.13901°
Mean motion
3.82477 °/min
Orbital period
94.12 mins
BSTAR
0.00020834
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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-S4 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-10 11:09:12.357Z | 253.87° W | 2026-10-10 11:12:12.357Z | 298.605° NW | 68.188° | 2026-10-10 11:16:12.357Z | 64.265° ENE |
| 5 mins | 2026-10-10 12:49:12.357Z | 298.884° NW | 2026-10-10 12:51:12.357Z | 348.399° N | 36.081° | 2026-10-10 12:54:12.357Z | 60.79° ENE |
| 5 mins | 2026-10-10 14:28:12.357Z | 306.031° NW | 2026-10-10 14:30:12.357Z | 359.866° N | 50.284° | 2026-10-10 14:33:12.357Z | 88.766° E |
| 5 mins | 2026-10-10 16:07:12.357Z | 269.007° W | 2026-10-10 16:09:12.357Z | 203.394° SW | 41.202° | 2026-10-10 16:12:12.357Z | 142.863° SSE |
| 4 mins | 2026-10-11 09:02:12.357Z | 176.864° S | 2026-10-11 09:04:12.357Z | 131.747° SE | 21.549° | 2026-10-11 09:06:12.357Z | 95.386° ESE |
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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