View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 26863U 01029A 25192.40687507 -.00000225 00000-0 00000-0 0 9993
2 26863 14.5922 9.0330 0015853 165.3497 204.4128 0.99291914 40472
Epoch (UTC): | 11 July 2025 09:45:54 |
Eccentricity: | 0.0015853 |
inclination: | 14.5922° |
perigee height: | 35996 km |
apogee height: | 36130 km |
right ascension of ascending node: | 9.0330° |
argument of perigee: | 165.3497° |
revolutions per day: | 0.99291914 |
mean anomaly at epoch: | 204.4128° |
orbit number at epoch: | 4047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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