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 55165U 26145.33218854 +.00000000 +00000-0 +60041-3 0 00001
2 55165 87.8957 355.1347 0001890 88.1768 271.9577 13.12927867 06
| Epoch (UTC): | 25 May 2026 07:58:21 |
| Eccentricity: | 0.0001890 |
| inclination: | 87.8957° |
| perigee height: | 1210 km |
| apogee height: | 1213 km |
| right ascension of ascending node: | 355.1347° |
| argument of perigee: | 88.1768° |
| revolutions per day: | 13.12927867 |
| mean anomaly at epoch: | 271.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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