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, 1.1 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 ION SCV-019
1 68435U 26067V 26217.44154192 .00002870 00000-0 13650-3 0 9990
2 68435 97.4580 175.3591 0008291 219.8044 140.2583 15.19965167 19429Epoch: 2026-08-05T10:35Z
TLE epoch observation values (Epoch: 2026-08-05T10:35:49.221Z)
Latitude
-0.00011°
Longitude
62.40813°
Altitude
513.426 km
Speed
7.605 km/s
True Right ascension
11h 41m 26s
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
14:25:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.619 km
Perigee altitude
497.209 km
Semi-major axis
6,881.051 km
Eccentricity
0.00083
Inclination
97.458°
RAAN
175.3591°
Arg. of periapsis
219.8044°
True anomaly
140.31899°
Mean anomaly
140.2583°
Eccentric anomaly
140.28865°
Mean motion
3.80243 °/min
Orbital period
94.68 mins
BSTAR
0.0001365
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-06 09:17:57.006Z | 52.617° ENE | 2026-08-06 09:19:57.006Z | 89.26° E | 18.222° | 2026-08-06 09:21:57.006Z | 129.84° SE |
| 4 mins | 2026-08-06 10:52:57.006Z | 316.243° NNW | 2026-08-06 10:53:57.006Z | 290.889° WNW | 22.537° | 2026-08-06 10:56:57.006Z | 234.721° WSW |
| 5 mins | 2026-08-06 21:29:57.006Z | 184.528° SSW | 2026-08-06 21:31:57.006Z | 264.923° W | 41.83° | 2026-08-06 21:34:57.006Z | 339.673° 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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