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 is defined by the following mean orbital elements,
1 27597U 26021.89989314 +.00000000 +00000-0 +28941-3 0 00002
2 27597 98.7695 340.0794 0001899 108.9734 251.1653 14.29243015 06
| Epoch (UTC): | 21 January 2026 21:35:50 |
| Eccentricity: | 0.0001899 |
| inclination: | 98.7695° |
| perigee height: | 793 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 340.0794° |
| argument of perigee: | 108.9734° |
| revolutions per day: | 14.29243015 |
| mean anomaly at epoch: | 251.1653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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