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 55359U 26145.26059076 +.00000000 +00000-0 +44920-4 0 00006
2 55359 43.0025 234.4075 0001473 268.5334 91.5349 15.27582927 03
| Epoch (UTC): | 25 May 2026 06:15:15 |
| Eccentricity: | 0.0001473 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 234.4075° |
| argument of perigee: | 268.5334° |
| revolutions per day: | 15.27582927 |
| mean anomaly at epoch: | 91.5349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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