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 65060U 26145.45221322 +.00000000 +00000-0 -23102-3 0 00001
2 65060 97.4493 222.5583 0002431 132.3457 227.7976 15.05649597 08
| Epoch (UTC): | 25 May 2026 10:51:11 |
| Eccentricity: | 0.0002431 |
| inclination: | 97.4493° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.5583° |
| argument of perigee: | 132.3457° |
| revolutions per day: | 15.05649597 |
| mean anomaly at epoch: | 227.7976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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