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 54097U 26144.91743816 +.00000000 +00000-0 +28566-4 0 00005
2 54097 53.2160 326.8492 0001289 90.2757 269.8383 15.08837395 06
| Epoch (UTC): | 24 May 2026 22:01:06 |
| Eccentricity: | 0.0001289 |
| inclination: | 53.2160° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 326.8492° |
| argument of perigee: | 90.2757° |
| revolutions per day: | 15.08837395 |
| mean anomaly at epoch: | 269.8383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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