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 55941U 26145.24372169 +.00000000 +00000-0 -20071-3 0 00003
2 55941 69.9994 91.5832 0003042 269.3268 90.7543 14.98334793 04
| Epoch (UTC): | 25 May 2026 05:50:57 |
| Eccentricity: | 0.0003042 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.5832° |
| argument of perigee: | 269.3268° |
| revolutions per day: | 14.98334793 |
| mean anomaly at epoch: | 90.7543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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