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 23089.79806636 .00000300 00000-0 15090-3 0 9998
2 25397 98.8600 46.6160 0001768 39.9159 320.2149 14.23848575284170
| Epoch (UTC): | 30 March 2023 19:09:12 |
| Eccentricity: | 0.0001768 |
| inclination: | 98.8600° |
| perigee height: | 811 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 46.6160° |
| argument of perigee: | 39.9159° |
| revolutions per day: | 14.23848575 |
| mean anomaly at epoch: | 320.2149° |
| orbit number at epoch: | 28417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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