ION SCV-019, 68435
Orbit data source: Space-Track
ION SCV-019, 68435 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Mon, 30 Mar 2026 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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68435 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
D-ORBIT
Mission
Operational Commercial Technology
Bus & Motor
ION-SC, PM200
Mass
220 kg wet, 150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ION SCV-019
1 68435U 26067V 26263.19164896 .00002734 00000-0 12911-3 0 9993
2 68435 97.4657 220.6206 0011341 72.2851 287.9621 15.20235447 26375Epoch: 2026-09-20T04:35Z
TLE epoch observation values (Epoch: 2026-09-20T04:35:58.470Z)
Latitude
-0.00001°
Longitude
152.53761°
Altitude
505.819 km
Speed
7.613 km/s
True Right ascension
14h 42m 28s
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
03:11:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.901 km
Perigee altitude
494.295 km
Semi-major axis
6,880.235 km
Eccentricity
0.00113
Inclination
97.4657°
RAAN
220.6206°
Arg. of periapsis
72.2851°
True anomaly
287.83842°
Mean anomaly
287.9621°
Eccentric anomaly
287.90027°
Mean motion
3.8031 °/min
Orbital period
94.66 mins
BSTAR
0.00012911
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.ION SCV-019 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 | 2026-09-20 20:32:25.993Z | 118.712° SE | 2026-09-20 20:35:25.993Z | 59.143° ENE | 21.766° | 2026-09-20 20:37:25.993Z | 22.744° NE |
| 4 mins | 2026-09-20 22:07:25.993Z | 235.153° WSW | 2026-09-20 22:08:25.993Z | 256.901° W | 20.97° | 2026-09-20 22:11:25.993Z | 314.267° NW |
| 4 mins | 2026-09-21 09:37:25.993Z | 52.273° ENE | 2026-09-21 09:39:25.993Z | 110.934° ESE | 31.263° | 2026-09-21 09:41:25.993Z | 153.804° 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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