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 23087.47909758 .00000261 00000-0 13369-3 0 9993
2 25397 98.8598 44.2799 0001865 43.9125 316.2201 14.23846885283843
| Epoch (UTC): | 28 March 2023 11:29:54 |
| Eccentricity: | 0.0001865 |
| inclination: | 98.8598° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 44.2799° |
| argument of perigee: | 43.9125° |
| revolutions per day: | 14.23846885 |
| mean anomaly at epoch: | 316.2201° |
| orbit number at epoch: | 28384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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