ICEYE-X79, 69870
Orbit data source: Space-Track
ICEYE-X79, 69870 is a payload satellite owned by RNAF (NL) 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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69870 intel report (Beta)
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Identifier
Orbit
Country
NL / NETHRelated business
Manufacturer
ICEYE
Mission
Operational spacecraft
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
BOX + PAN, 0.8 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ICEYE-X79
1 69870U 26156B 26211.28362762 .00002783 00000-0 28194-3 0 9995
2 69870 97.7504 111.3515 0008533 75.3078 284.9086 14.91702368 3427Epoch: 2026-07-30T06:48Z
TLE epoch observation values (Epoch: 2026-07-30T06:48:25.426Z)
Latitude
-0.00002°
Longitude
61.3192°
Altitude
594.143 km
Speed
7.564 km/s
True Right ascension
07h 25m 24s
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
12:33:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.591 km
Perigee altitude
583.7 km
Semi-major axis
6,967.783 km
Eccentricity
0.00085
Inclination
97.7504°
RAAN
111.3515°
Arg. of periapsis
75.3078°
True anomaly
284.81408°
Mean anomaly
284.9086°
Eccentric anomaly
284.86134°
Mean motion
3.73165 °/min
Orbital period
96.47 mins
BSTAR
0.00028194
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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.ICEYE-X79 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 05:55:03.674Z | 27.372° NE | 2026-07-31 05:58:03.674Z | 85.401° E | 36.46° | 2026-07-31 06:02:03.674Z | 173.83° S |
| 5 mins | 2026-07-31 16:46:03.674Z | 118.517° SE | 2026-07-31 16:48:03.674Z | 75.769° E | 26.784° | 2026-07-31 16:51:03.674Z | 15.472° NNE |
| 4 mins | 2026-07-31 18:22:03.674Z | 233.335° WSW | 2026-07-31 18:24:03.674Z | 270.464° WNW | 18.815° | 2026-07-31 18:26:03.674Z | 304.589° NW |
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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