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 65066U 26145.57682457 +.00000000 +00000-0 +40964-3 0 00004
2 65066 97.4493 222.7016 0002621 186.7992 173.3200 15.05657709 05
| Epoch (UTC): | 25 May 2026 13:50:37 |
| Eccentricity: | 0.0002621 |
| inclination: | 97.4493° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.7016° |
| argument of perigee: | 186.7992° |
| revolutions per day: | 15.05657709 |
| mean anomaly at epoch: | 173.3200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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