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 55811U 26145.65763928 +.00000000 +00000-0 -15255-3 0 00009
2 55811 87.8944 294.1962 0001250 68.6443 291.4820 13.14504141 04
| Epoch (UTC): | 25 May 2026 15:47:00 |
| Eccentricity: | 0.0001250 |
| inclination: | 87.8944° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.1962° |
| argument of perigee: | 68.6443° |
| revolutions per day: | 13.14504141 |
| mean anomaly at epoch: | 291.4820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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