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 64541U 26145.57670198 +.00000000 +00000-0 +13302-3 0 00006
2 64541 97.4672 260.4469 0001541 251.6643 108.4424 15.20105546 08
| Epoch (UTC): | 25 May 2026 13:50:27 |
| Eccentricity: | 0.0001541 |
| inclination: | 97.4672° |
| perigee height: | 504 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 260.4469° |
| argument of perigee: | 251.6643° |
| revolutions per day: | 15.20105546 |
| mean anomaly at epoch: | 108.4424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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