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 27597U 02056A 25196.81883686 .00000193 00000-0 94079-4 0 9990
2 27597 98.7390 149.2130 0001219 34.2792 325.8468 14.29067462176469
| Epoch (UTC): | 15 July 2025 19:39:07 |
| Eccentricity: | 0.0001219 |
| inclination: | 98.7390° |
| perigee height: | 794 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 149.2130° |
| argument of perigee: | 34.2792° |
| revolutions per day: | 14.29067462 |
| mean anomaly at epoch: | 325.8468° |
| orbit number at epoch: | 17646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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