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 47857U 26145.63933712 +.00000000 +00000-0 +21927-3 0 00000
2 47857 63.4074 316.0166 0172809 0.3980 359.7153 13.45446337 00
| Epoch (UTC): | 25 May 2026 15:20:38 |
| Eccentricity: | 0.0172809 |
| inclination: | 63.4074° |
| perigee height: | 960 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 316.0166° |
| argument of perigee: | 0.3980° |
| revolutions per day: | 13.45446337 |
| mean anomaly at epoch: | 359.7153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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