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 55773U 26145.08030211 +.00000000 +00000-0 -13392-4 0 00006
2 55773 69.9999 31.9324 0002587 270.1795 89.9067 14.98329458 07
| Epoch (UTC): | 25 May 2026 01:55:38 |
| Eccentricity: | 0.0002587 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.9324° |
| argument of perigee: | 270.1795° |
| revolutions per day: | 14.98329458 |
| mean anomaly at epoch: | 89.9067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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