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 65172U 26145.57917610 +.00000000 +00000-0 +12843-3 0 00009
2 65172 86.4912 259.5532 0001878 94.4894 265.6455 13.24404187 03
| Epoch (UTC): | 25 May 2026 13:54:00 |
| Eccentricity: | 0.0001878 |
| inclination: | 86.4912° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.5532° |
| argument of perigee: | 94.4894° |
| revolutions per day: | 13.24404187 |
| mean anomaly at epoch: | 265.6455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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