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 55315U 26145.56198411 +.00000000 +00000-0 +19204-6 0 00007
2 55315 69.9987 190.6413 0004048 268.1227 91.9468 14.98331967 05
| Epoch (UTC): | 25 May 2026 13:29:15 |
| Eccentricity: | 0.0004048 |
| inclination: | 69.9987° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.6413° |
| argument of perigee: | 268.1227° |
| revolutions per day: | 14.98331967 |
| mean anomaly at epoch: | 91.9468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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