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 55935U 26145.29796045 +.00000000 +00000-0 -16038-3 0 00002
2 55935 69.9998 91.3716 0003297 268.2453 91.8328 14.98340352 07
| Epoch (UTC): | 25 May 2026 07:09:03 |
| Eccentricity: | 0.0003297 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.3716° |
| argument of perigee: | 268.2453° |
| revolutions per day: | 14.98340352 |
| mean anomaly at epoch: | 91.8328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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