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 65170U 26145.57164104 +.00000000 +00000-0 +13462-3 0 00007
2 65170 86.4913 259.5512 0001861 92.4247 267.7100 13.24404397 05
| Epoch (UTC): | 25 May 2026 13:43:09 |
| Eccentricity: | 0.0001861 |
| inclination: | 86.4913° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.5512° |
| argument of perigee: | 92.4247° |
| revolutions per day: | 13.24404397 |
| mean anomaly at epoch: | 267.7100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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