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 25082.92591564 .00000445 00000-0 21301-3 0 9991
2 25397 98.9637 60.4534 0002383 79.9433 280.2013 14.24280294387238
| Epoch (UTC): | 23 March 2025 22:13:19 |
| Eccentricity: | 0.0002383 |
| inclination: | 98.9637° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 60.4534° |
| argument of perigee: | 79.9433° |
| revolutions per day: | 14.24280294 |
| mean anomaly at epoch: | 280.2013° |
| orbit number at epoch: | 38723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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