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 64905U 26145.58335647 +.00000000 +00000-0 +23353-2 0 00004
2 64905 53.1590 348.6412 0000826 72.4072 322.4469 15.33443291 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000826 |
| inclination: | 53.1590° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 348.6412° |
| argument of perigee: | 72.4072° |
| revolutions per day: | 15.33443291 |
| mean anomaly at epoch: | 322.4469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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