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 23080.31136032 .00000197 00000-0 10592-3 0 9999
2 25397 98.8588 37.0600 0002114 56.2134 303.9245 14.23842363283048
| Epoch (UTC): | 21 March 2023 07:28:21 |
| Eccentricity: | 0.0002114 |
| inclination: | 98.8588° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 37.0600° |
| argument of perigee: | 56.2134° |
| revolutions per day: | 14.23842363 |
| mean anomaly at epoch: | 303.9245° |
| orbit number at epoch: | 28304 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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