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 23342.48653155 .00000100 00000-0 63678-4 0 9996
2 25397 98.8950 301.6562 0001605 34.5716 325.5566 14.23953922320139
| Epoch (UTC): | 08 December 2023 11:40:36 |
| Eccentricity: | 0.0001605 |
| inclination: | 98.8950° |
| perigee height: | 811 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 301.6562° |
| argument of perigee: | 34.5716° |
| revolutions per day: | 14.23953922 |
| mean anomaly at epoch: | 325.5566° |
| orbit number at epoch: | 32013 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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