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 25397U 98043D 23272.85151929 .00000193 00000-0 10400-3 0 9997
2 25397 98.8811 231.2667 0001424 147.2210 212.9057 14.23915535310444
Epoch (UTC): | 29 September 2023 20:26:11 |
Eccentricity: | 0.0001424 |
inclination: | 98.8811° |
perigee height: | 811 km |
apogee height: | 813 km |
right ascension of ascending node: | 231.2667° |
argument of perigee: | 147.2210° |
revolutions per day: | 14.23915535 |
mean anomaly at epoch: | 212.9057° |
orbit number at epoch: | 31044 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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