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 65062U 26145.20853751 +.00000000 +00000-0 +49345-3 0 00009
2 65062 97.4473 222.2719 0002908 129.7176 230.4307 15.05657168 05
| Epoch (UTC): | 25 May 2026 05:00:17 |
| Eccentricity: | 0.0002908 |
| inclination: | 97.4473° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 222.2719° |
| argument of perigee: | 129.7176° |
| revolutions per day: | 15.05657168 |
| mean anomaly at epoch: | 230.4307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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