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 65166U 26145.61696395 +.00000000 +00000-0 +21794-4 0 00007
2 65166 86.4952 259.6194 0001871 94.5071 265.6277 13.24403988 06
| Epoch (UTC): | 25 May 2026 14:48:25 |
| Eccentricity: | 0.0001871 |
| inclination: | 86.4952° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.6194° |
| argument of perigee: | 94.5071° |
| revolutions per day: | 13.24403988 |
| mean anomaly at epoch: | 265.6277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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