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 26053.61260527 +.00000000 +00000-0 +12105-3 0 00000
2 27597 98.7742 11.9887 0002025 64.3810 295.7580 14.29272559 06
| Epoch (UTC): | 22 February 2026 14:42:09 |
| Eccentricity: | 0.0002025 |
| inclination: | 98.7742° |
| perigee height: | 793 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 11.9887° |
| argument of perigee: | 64.3810° |
| revolutions per day: | 14.29272559 |
| mean anomaly at epoch: | 295.7580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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