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 65594U 26145.47377382 +.00000000 +00000-0 +58934-3 0 00003
2 65594 97.4522 213.9493 0002132 133.8289 226.3115 15.05667400 07
| Epoch (UTC): | 25 May 2026 11:22:14 |
| Eccentricity: | 0.0002132 |
| inclination: | 97.4522° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.9493° |
| argument of perigee: | 133.8289° |
| revolutions per day: | 15.05667400 |
| mean anomaly at epoch: | 226.3115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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