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 55933U 26145.30213765 +.00000000 +00000-0 -15203-4 0 00009
2 55933 69.9999 91.3887 0003099 267.4330 92.6474 14.98331717 06
| Epoch (UTC): | 25 May 2026 07:15:04 |
| Eccentricity: | 0.0003099 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.3887° |
| argument of perigee: | 267.4330° |
| revolutions per day: | 14.98331717 |
| mean anomaly at epoch: | 92.6474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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