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 65422U 26145.63149897 +.00000000 +00000-0 +32622-3 0 00005
2 65422 53.1620 235.0079 0000422 93.0782 267.0268 15.30205269 05
| Epoch (UTC): | 25 May 2026 15:09:21 |
| Eccentricity: | 0.0000422 |
| inclination: | 53.1620° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 235.0079° |
| argument of perigee: | 93.0782° |
| revolutions per day: | 15.30205269 |
| mean anomaly at epoch: | 267.0268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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