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 55791U 26145.05503184 +.00000000 +00000-0 +61098-4 0 00002
2 55791 69.9996 11.9677 0002666 267.9151 92.1703 14.98331203 05
| Epoch (UTC): | 25 May 2026 01:19:14 |
| Eccentricity: | 0.0002666 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.9677° |
| argument of perigee: | 267.9151° |
| revolutions per day: | 14.98331203 |
| mean anomaly at epoch: | 92.1703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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