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 55999U 26145.55812450 +.00000000 +00000-0 +65461-4 0 00004
2 55999 43.0045 345.6508 0001642 268.0721 91.9942 15.27580230 02
| Epoch (UTC): | 25 May 2026 13:23:41 |
| Eccentricity: | 0.0001642 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.6508° |
| argument of perigee: | 268.0721° |
| revolutions per day: | 15.27580230 |
| mean anomaly at epoch: | 91.9942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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