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 23092.11703289 .00000249 00000-0 12848-3 0 9998
2 25397 98.8604 48.9523 0001665 35.6843 324.4446 14.23849718284728
| Epoch (UTC): | 02 April 2023 02:48:31 |
| Eccentricity: | 0.0001665 |
| inclination: | 98.8604° |
| perigee height: | 811 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 48.9523° |
| argument of perigee: | 35.6843° |
| revolutions per day: | 14.23849718 |
| mean anomaly at epoch: | 324.4446° |
| orbit number at epoch: | 28472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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