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 64773U 26145.56409372 +.00000000 +00000-0 +36360-3 0 00005
2 64773 53.1582 244.8203 0001633 92.6886 267.4303 15.34399949 09
| Epoch (UTC): | 25 May 2026 13:32:17 |
| Eccentricity: | 0.0001633 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 244.8203° |
| argument of perigee: | 92.6886° |
| revolutions per day: | 15.34399949 |
| mean anomaly at epoch: | 267.4303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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