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 55405U 26145.52489740 +.00000000 +00000-0 +20220-4 0 00009
2 55405 69.9993 230.7621 0003682 269.1119 90.9619 14.98332544 02
| Epoch (UTC): | 25 May 2026 12:35:51 |
| Eccentricity: | 0.0003682 |
| inclination: | 69.9993° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 230.7621° |
| argument of perigee: | 269.1119° |
| revolutions per day: | 14.98332544 |
| mean anomaly at epoch: | 90.9619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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