RAVEN, 69016
AKA "RAVEN" on Space-Track | Orbit data source: Space-Track
RAVEN, 69016 is a German payload satellite in SSO that was launched on Sun, 03 May 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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69016 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
None
Manufacturer
Endurosat
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~8 kg wet, ~8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 RAVEN
1 69016U 26100AN 26175.16581287 .00002143 00000-0 98550-4 0 9991
2 69016 97.4027 72.9282 0008968 36.5112 323.6734 15.21395633 7870Epoch: 2026-06-24T03:58Z
TLE epoch observation values (Epoch: 2026-06-24T03:58:46.231Z)
Latitude
-0.00003°
Longitude
100.90864°
Altitude
499.752 km
Speed
7.617 km/s
True Right ascension
04h 51m 42s
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
08:54:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.761 km
Perigee altitude
492.427 km
Semi-major axis
6,876.731 km
Eccentricity
0.0009
Inclination
97.4027°
RAAN
72.9282°
Arg. of periapsis
36.5112°
True anomaly
323.61247°
Mean anomaly
323.6734°
Eccentric anomaly
323.64294°
Mean motion
3.80601 °/min
Orbital period
94.59 mins
BSTAR
0.00009855
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.RAVEN 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-25 05:48:19.132Z | 26.633° NE | 2026-06-25 05:51:19.132Z | 122.365° SE | 37.414° | 2026-06-25 05:54:19.132Z | 176.564° S |
| 4 mins | 2026-06-25 18:00:19.132Z | 226.186° WSW | 2026-06-25 18:02:19.132Z | 272.19° WNW | 20.997° | 2026-06-25 18:04:19.132Z | 311.38° NW |
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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