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 61535U 26145.37565125 +.00000000 +00000-0 +97622-5 0 00006
2 61535 53.1590 218.0872 0001135 87.3241 272.7907 15.69708717 03
| Epoch (UTC): | 25 May 2026 09:00:56 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.1590° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 218.0872° |
| argument of perigee: | 87.3241° |
| revolutions per day: | 15.69708717 |
| mean anomaly at epoch: | 272.7907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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