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: 12 hours ago
TLE from 12 hours ago
0 TOMORROW-S4
1 62386U 24247K 26171.33708435 .00004744 00000-0 17481-3 0 9997
2 62386 44.9827 275.8397 0002509 26.1390 333.9619 15.29165199 83439Epoch: 2026-06-20T08:05Z
TLE epoch observation values (Epoch: 2026-06-20T08:05:24.087Z)
Latitude
-0.00008°
Longitude
-114.0639°
Altitude
476.758 km
Speed
7.63 km/s
True Right ascension
18h 23m 21s
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
07:18:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.64 km
Perigee altitude
478.199 km
Semi-major axis
6,858.057 km
Eccentricity
0.00025
Inclination
44.9827°
RAAN
275.8397°
Arg. of periapsis
26.139°
True anomaly
333.94928°
Mean anomaly
333.9619°
Eccentric anomaly
333.95559°
Mean motion
3.82157 °/min
Orbital period
94.2 mins
BSTAR
0.00017481
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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 | 2026-06-21 09:21:04.666Z | 194.295° SSW | 2026-06-21 09:24:04.666Z | 136.152° SSE | 21.353° | 2026-06-21 09:26:04.666Z | 96.738° ESE |
| 5 mins | 2026-06-21 11:00:04.666Z | 255.815° W | 2026-06-21 11:02:04.666Z | 308.355° NW | 43.659° | 2026-06-21 11:05:04.666Z | 63.124° ENE |
| 5 mins | 2026-06-21 12:39:04.666Z | 298.679° NW | 2026-06-21 12:41:04.666Z | 349.619° N | 30.741° | 2026-06-21 12:44:04.666Z | 61.393° ENE |
| 5 mins | 2026-06-21 14:18:04.666Z | 305.26° NW | 2026-06-21 14:20:04.666Z | 357.121° N | 37.475° | 2026-06-21 14:23:04.666Z | 88.638° E |
| 5 mins | 2026-06-21 15:57:04.666Z | 270.493° WNW | 2026-06-21 15:59:04.666Z | 208.941° SW | 33.417° | 2026-06-21 16:02:04.666Z | 143.499° 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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