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 55295U 26145.33690992 +.00000000 +00000-0 +19365-4 0 00006
2 55295 69.9990 211.3301 0003908 268.9357 91.1354 14.98331024 09
| Epoch (UTC): | 25 May 2026 08:05:09 |
| Eccentricity: | 0.0003908 |
| inclination: | 69.9990° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 211.3301° |
| argument of perigee: | 268.9357° |
| revolutions per day: | 14.98331024 |
| mean anomaly at epoch: | 91.1354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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