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 23090.85214238 .00000279 00000-0 14157-3 0 9996
2 25397 98.8601 47.6779 0001722 38.1183 322.0117 14.23849113284541
| Epoch (UTC): | 31 March 2023 20:27:05 |
| Eccentricity: | 0.0001722 |
| inclination: | 98.8601° |
| perigee height: | 811 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 47.6779° |
| argument of perigee: | 38.1183° |
| revolutions per day: | 14.23849113 |
| mean anomaly at epoch: | 322.0117° |
| orbit number at epoch: | 28454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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