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 26033.45095949 +.00000000 +00000-0 +15260-3 0 00009
2 27597 98.7708 351.6997 0002115 92.3416 267.8007 14.29256351 03
| Epoch (UTC): | 02 February 2026 10:49:22 |
| Eccentricity: | 0.0002115 |
| inclination: | 98.7708° |
| perigee height: | 793 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 351.6997° |
| argument of perigee: | 92.3416° |
| revolutions per day: | 14.29256351 |
| mean anomaly at epoch: | 267.8007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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