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 36095U 09063A 25198.52701656 -.00000052 00000-0 17023-4 0 9993
2 36095 67.1492 346.7650 0007195 293.3435 66.6892 13.97006933798570
Epoch (UTC): | 17 July 2025 12:38:54 |
Eccentricity: | 0.0007195 |
inclination: | 67.1492° |
perigee height: | 899 km |
apogee height: | 909 km |
right ascension of ascending node: | 346.7650° |
argument of perigee: | 293.3435° |
revolutions per day: | 13.97006933 |
mean anomaly at epoch: | 66.6892° |
orbit number at epoch: | 79857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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