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 26019.30963683 +.00000000 +00000-0 +13762-3 0 00001
2 27597 98.7690 337.4739 0001838 112.2418 247.8959 14.29238098 06
| Epoch (UTC): | 19 January 2026 07:25:52 |
| Eccentricity: | 0.0001838 |
| inclination: | 98.7690° |
| perigee height: | 793 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 337.4739° |
| argument of perigee: | 112.2418° |
| revolutions per day: | 14.29238098 |
| mean anomaly at epoch: | 247.8959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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