ION SCV-023, 69876
Orbit data source: Space-Track
ION SCV-023, 69876 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Tue, 07 Jul 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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69876 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
D-ORBIT
Mission
Operational spacecraft
Bus & Motor
ION-SC, PM200
Mass
220 kg wet, 150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
BOX, 0.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ION SCV-023
1 69876U 26156H 26210.27382809 -.00002436 00000-0 -23559-3 0 9990
2 69876 97.6856 110.3202 0009045 90.7932 269.4324 14.91889285 3273Epoch: 2026-07-29T06:34Z
TLE epoch observation values (Epoch: 2026-07-29T06:34:18.746Z)
Latitude
-0°
Longitude
64.81103°
Altitude
595.157 km
Speed
7.562 km/s
True Right ascension
07h 21m 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
10:38:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.362 km
Perigee altitude
582.759 km
Semi-major axis
6,967.197 km
Eccentricity
0.0009
Inclination
97.6856°
RAAN
110.3202°
Arg. of periapsis
90.7932°
True anomaly
269.32876°
Mean anomaly
269.4324°
Eccentric anomaly
269.38058°
Mean motion
3.73212 °/min
Orbital period
96.46 mins
BSTAR
-0.00023559
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Other satellites on launch #156 in the year 2026 (2026-07-07 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-023 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-07-31 05:49:25.917Z | 29.613° NE | 2026-07-31 05:52:25.917Z | 82.233° E | 33.13° | 2026-07-31 05:56:25.917Z | 168.783° S |
| 5 mins | 2026-07-31 16:40:25.917Z | 115.398° SE | 2026-07-31 16:42:25.917Z | 76.946° E | 23.947° | 2026-07-31 16:45:25.917Z | 19.133° NNE |
| 5 mins | 2026-07-31 18:16:25.917Z | 229.34° WSW | 2026-07-31 18:18:25.917Z | 269.579° W | 21.26° | 2026-07-31 18:21:25.917Z | 317.457° NNW |
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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