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: 14 hours ago
TLE from 14 hours ago
0 TOMORROW-S4
1 62386U 24247K 26219.73458700 .00003265 00000-0 12151-3 0 9997
2 62386 44.9836 10.7932 0004724 310.3731 49.6740 15.29741828 90846Epoch: 2026-08-07T17:37Z
TLE epoch observation values (Epoch: 2026-08-07T17:37:48.316Z)
Latitude
-0.00002°
Longitude
150.08583°
Altitude
474.486 km
Speed
7.632 km/s
True Right ascension
00h 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
21:28:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.436 km
Perigee altitude
474.958 km
Semi-major axis
6,856.334 km
Eccentricity
0.00047
Inclination
44.9836°
RAAN
10.7932°
Arg. of periapsis
310.3731°
True anomaly
49.71529°
Mean anomaly
49.674°
Eccentric anomaly
49.69464°
Mean motion
3.82301 °/min
Orbital period
94.17 mins
BSTAR
0.00012151
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-08 12:37:03.651Z | 191.158° SSW | 2026-08-08 12:39:03.651Z | 154.68° SSE | 20.994° | 2026-08-08 12:42:03.651Z | 93.332° ESE |
| 5 mins | 2026-08-08 14:16:03.651Z | 257.144° W | 2026-08-08 14:18:03.651Z | 5.871° NNE | 43.742° | 2026-08-08 14:21:03.651Z | 63.797° ENE |
| 5 mins | 2026-08-08 15:55:03.651Z | 303.601° NW | 2026-08-08 15:57:03.651Z | 4.352° NNE | 30.77° | 2026-08-08 16:00:03.651Z | 64.058° ENE |
| 5 mins | 2026-08-08 17:34:03.651Z | 309.183° NW | 2026-08-08 17:36:03.651Z | 22.812° NE | 37.975° | 2026-08-08 17:39:03.651Z | 90.726° ESE |
| 5 mins | 2026-08-08 19:13:03.651Z | 263.963° W | 2026-08-08 19:15:03.651Z | 189.632° SSW | 32.241° | 2026-08-08 19:18:03.651Z | 141.045° 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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