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REPLICATOR-2, 69927

Orbit data source: Space-Track

REPLICATOR-2, 69927 is a German payload satellite 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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Identifier
69927, 2026-156BL
Orbit
SSO
Country
Flag of DEDE / GER
Related business
None
Manufacturer
ORBMAT
Mission
Operational spacecraft
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2026-07-07 (3 weeks 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
RCS unknown

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 REPLICATOR-2
1 69927U 26156BL  26211.27519751  .00001295  00000-0  13247-3 0  9999
2 69927  97.7524 111.3705 0009933  84.6547 275.5805 14.92222109  3259
Epoch: 2026-07-30T06:36Z
TLE epoch observation values (Epoch: 2026-07-30T06:36:17.064Z)
Latitude
-0.00006°
Longitude
64.38135°
Altitude
593.384 km
Speed
7.564 km/s
True Right ascension
07h 25m 28s
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
11:16:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.946 km
Perigee altitude
581.107 km
Semi-major axis
6,966.163 km
Eccentricity
0.00099
Inclination
97.7524°
RAAN
111.3705°
Arg. of periapsis
84.6547°
True anomaly
275.4672°
Mean anomaly
275.5805°
Eccentric anomaly
275.52385°
Mean motion
3.73295 °/min
Orbital period
96.44 mins
BSTAR
0.00013247
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