FLAMINGO-1, 67391
Orbit data source: Space-Track
FLAMINGO-1, 67391 is a German payload satellite in SSO that was launched on Sun, 11 Jan 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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67391 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
Endurosat
Mission
Operational Commercial Technology
Bus & Motor
ESPASAT, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.475 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FLAMINGO-1
1 67391U 26004AE 26264.47590664 .00001227 00000-0 63802-4 0 9994
2 67391 97.4620 261.9757 0005848 10.2308 349.9044 15.17932513 38351Epoch: 2026-09-21T11:25Z
TLE epoch observation values (Epoch: 2026-09-21T11:25:18.333Z)
Latitude
-0.00002°
Longitude
90.29412°
Altitude
511.208 km
Speed
7.61 km/s
True Right ascension
17h 27m 54s
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
15:39:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.089 km
Perigee altitude
505.033 km
Semi-major axis
6,887.198 km
Eccentricity
0.00058
Inclination
97.462°
RAAN
261.9757°
Arg. of periapsis
10.2308°
True anomaly
349.89264°
Mean anomaly
349.9044°
Eccentric anomaly
349.89852°
Mean motion
3.79734 °/min
Orbital period
94.8 mins
BSTAR
0.000063802
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Other satellites on launch #4 in the year 2026 (2026-01-11 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.FLAMINGO-1 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 | 2026-09-22 00:12:26.667Z | 182.624° SSW | 2026-09-22 00:15:26.667Z | 283.956° WNW | 56.798° | 2026-09-22 00:18:26.667Z | 339.016° N |
| 5 mins | 2026-09-22 13:18:26.667Z | 343.537° N | 2026-09-22 13:20:26.667Z | 291.828° WNW | 37.123° | 2026-09-22 13:23:26.667Z | 223.135° SW |
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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