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 08860U 26106.83855358 +.00000000 +00000-0 +10465-3 0 00004
2 08860 99.9119 318.5588 0041970 152.9854 218.5836 13.68287069 08
| Epoch (UTC): | 16 April 2026 20:07:31 |
| Eccentricity: | 0.0041970 |
| inclination: | 99.9119° |
| perigee height: | 975 km |
| apogee height: | 1037 km |
| right ascension of ascending node: | 318.5588° |
| argument of perigee: | 152.9854° |
| revolutions per day: | 13.68287069 |
| mean anomaly at epoch: | 218.5836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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