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 55272U 26145.38280110 +.00000000 +00000-0 -14145-3 0 00004
2 55272 69.9993 211.0933 0003606 270.3632 89.7114 14.98329358 07
| Epoch (UTC): | 25 May 2026 09:11:14 |
| Eccentricity: | 0.0003606 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 211.0933° |
| argument of perigee: | 270.3632° |
| revolutions per day: | 14.98329358 |
| mean anomaly at epoch: | 89.7114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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