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HELIOS, 69021

AKA "HELIOS" on Space-Track | Orbit data source: Space-Track

HELIOS, 69021 is a Greek 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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Identifier
69021, 2026-100AT
Orbit
SSO
Country
Flag of GRGR / GREC
Related business
Manufacturer
EMTECH
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
~8 kg wet, ~8 kg dry
Launch date (UTC)
2026-05-03 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 HELIOS
1 69021U 26100AT  26266.15873524  .00004520  00000-0  20623-3 0  9991
2 69021  97.3886 162.0939 0005251  26.5046 333.6457 15.21109125 21693
Epoch: 2026-09-23T03:48Z
TLE epoch observation values (Epoch: 2026-09-23T03:48:34.724Z)
Latitude
-0.00008°
Longitude
102.93536°
Altitude
502.348 km
Speed
7.615 km/s
True Right ascension
10h 48m 22s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:33:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.069 km
Perigee altitude
495.846 km
Semi-major axis
6,877.594 km
Eccentricity
0.00053
Inclination
97.3886°
RAAN
162.0939°
Arg. of periapsis
26.5046°
True anomaly
333.61897°
Mean anomaly
333.6457°
Eccentric anomaly
333.63234°
Mean motion
3.80529 °/min
Orbital period
94.61 mins
BSTAR
0.00020623
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Documentation

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