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 65430U 26145.55145272 +.00000000 +00000-0 +65819-3 0 00002
2 65430 53.1595 235.2196 0003055 76.2254 283.9088 15.34419641 01
| Epoch (UTC): | 25 May 2026 13:14:05 |
| Eccentricity: | 0.0003055 |
| inclination: | 53.1595° |
| perigee height: | 461 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 235.2196° |
| argument of perigee: | 76.2254° |
| revolutions per day: | 15.34419641 |
| mean anomaly at epoch: | 283.9088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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