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 65024U 26145.58335647 +.00000000 +00000-0 -48719-3 0 00002
2 65024 53.1593 296.7545 0000813 74.8888 32.6139 15.34387448 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000813 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 296.7545° |
| argument of perigee: | 74.8888° |
| revolutions per day: | 15.34387448 |
| mean anomaly at epoch: | 32.6139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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