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 65317U 26145.62844734 +.00000000 +00000-0 +13193-3 0 00001
2 65317 97.2035 221.3383 0000739 229.0376 131.0806 15.38554502 07
| Epoch (UTC): | 25 May 2026 15:04:57 |
| Eccentricity: | 0.0000739 |
| inclination: | 97.2035° |
| perigee height: | 450 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 221.3383° |
| argument of perigee: | 229.0376° |
| revolutions per day: | 15.38554502 |
| mean anomaly at epoch: | 131.0806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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