TOMORROW-S2, 60485
Orbit data source: Space-Track
TOMORROW-S2, 60485 is a payload satellite owned by Tomorrow.io (US) in SSO that was launched on Fri, 16 Aug 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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60485 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: 22 hours ago
TLE from 22 hours ago
0 TOMORROW-S2
1 60485U 24149T 26259.52870040 .00007176 00000-0 22100-3 0 9992
2 60485 97.3758 340.3378 0001573 341.3643 18.7542 15.33936055116085Epoch: 2026-09-16T12:41Z
TLE epoch observation values (Epoch: 2026-09-16T12:41:19.714Z)
Latitude
-0.00002°
Longitude
154.52667°
Altitude
466.173 km
Speed
7.634 km/s
True Right ascension
22h 41m 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
03:00:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.104 km
Perigee altitude
459.953 km
Semi-major axis
6,839.166 km
Eccentricity
0.00016
Inclination
97.3758°
RAAN
340.3378°
Arg. of periapsis
341.3643°
True anomaly
18.76°
Mean anomaly
18.7542°
Eccentric anomaly
18.7571°
Mean motion
3.83741 °/min
Orbital period
93.81 mins
BSTAR
0.000221
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-S2 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-17 17:26:55.512Z | 55.984° ENE | 2026-09-17 17:28:55.512Z | 91.761° ESE | 15.56° | 2026-09-17 17:30:55.512Z | 128.808° SE |
| 4 mins | 2026-09-17 19:00:55.512Z | 320.614° NNW | 2026-09-17 19:01:55.512Z | 292.755° NW | 26.635° | 2026-09-17 19:04:55.512Z | 230.673° WSW |
| 5 mins | 2026-09-18 05:31:55.512Z | 165.657° S | 2026-09-18 05:33:55.512Z | 153.202° SSE | 77.491° | 2026-09-18 05:36:55.512Z | 348.999° N |
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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