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 23266.45708488 .00000204 00000-0 10889-3 0 9998
2 25397 98.8796 224.8085 0001082 159.2771 200.8451 14.23912090309538
Epoch (UTC): | 23 September 2023 10:58:12 |
Eccentricity: | 0.0001082 |
inclination: | 98.8796° |
perigee height: | 811 km |
apogee height: | 813 km |
right ascension of ascending node: | 224.8085° |
argument of perigee: | 159.2771° |
revolutions per day: | 14.23912090 |
mean anomaly at epoch: | 200.8451° |
orbit number at epoch: | 30953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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