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 64734U 26145.36586535 +.00000000 +00000-0 +58226-3 0 00002
2 64734 53.1586 184.7246 0001619 77.7755 282.3426 15.30208488 07
| Epoch (UTC): | 25 May 2026 08:46:50 |
| Eccentricity: | 0.0001619 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.7246° |
| argument of perigee: | 77.7755° |
| revolutions per day: | 15.30208488 |
| mean anomaly at epoch: | 282.3426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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