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 61560U 26145.57334770 +.00000000 +00000-0 +13338-3 0 00006
2 61560 88.9836 57.7262 0009670 104.7834 255.4433 14.27517190 03
| Epoch (UTC): | 25 May 2026 13:45:37 |
| Eccentricity: | 0.0009670 |
| inclination: | 88.9836° |
| perigee height: | 793 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 57.7262° |
| argument of perigee: | 104.7834° |
| revolutions per day: | 14.27517190 |
| mean anomaly at epoch: | 255.4433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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