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: 2 days ago
TLE from 2 days ago
0 ION SCV-019
1 68435U 26067V 26258.84740965 .00003478 00000-0 16345-3 0 9997
2 68435 97.4651 216.3199 0011467 84.9674 275.2870 15.20209662 25717Epoch: 2026-09-15T20:20Z
TLE epoch observation values (Epoch: 2026-09-15T20:20:16.193Z)
Latitude
-0.00002°
Longitude
-83.55505°
Altitude
507.578 km
Speed
7.611 km/s
True Right ascension
14h 25m 16s
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
02:59:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.065 km
Perigee altitude
494.286 km
Semi-major axis
6,880.313 km
Eccentricity
0.00115
Inclination
97.4651°
RAAN
216.3199°
Arg. of periapsis
84.9674°
True anomaly
275.15614°
Mean anomaly
275.287°
Eccentric anomaly
275.22157°
Mean motion
3.80304 °/min
Orbital period
94.66 mins
BSTAR
0.00016345
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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 | 2026-09-17 10:48:33.828Z | 343.184° N | 2026-09-17 10:51:33.828Z | 279.463° WNW | 26.402° | 2026-09-17 10:53:33.828Z | 238.652° WSW |
| 6 mins | 2026-09-17 21:26:33.828Z | 176.728° S | 2026-09-17 21:28:33.828Z | 206.667° SW | 60.912° | 2026-09-17 21:32:33.828Z | 343.342° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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