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 61064U 26145.26905553 +.00000000 +00000-0 -14707-4 0 00007
2 61064 53.1613 95.3148 0001332 82.1887 277.9265 15.31692514 06
| Epoch (UTC): | 25 May 2026 06:27:26 |
| Eccentricity: | 0.0001332 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.3148° |
| argument of perigee: | 82.1887° |
| revolutions per day: | 15.31692514 |
| mean anomaly at epoch: | 277.9265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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