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 38770U 12048N 25198.59766423 .00027094 00000-0 51116-3 0 9996
2 38770 64.6412 323.2755 0090895 267.7159 91.3569 15.43899603 66659
Epoch (UTC): | 17 July 2025 14:20:38 |
Eccentricity: | 0.0090895 |
inclination: | 64.6412° |
perigee height: | 372 km |
apogee height: | 496 km |
right ascension of ascending node: | 323.2755° |
argument of perigee: | 267.7159° |
revolutions per day: | 15.43899603 |
mean anomaly at epoch: | 91.3569° |
orbit number at epoch: | 6665 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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