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 47856U 26145.63927802 +.00000000 +00000-0 -25652-4 0 00003
2 47856 63.4063 316.7268 0172751 0.5331 359.5848 13.45446237 03
| Epoch (UTC): | 25 May 2026 15:20:33 |
| Eccentricity: | 0.0172751 |
| inclination: | 63.4063° |
| perigee height: | 960 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 316.7268° |
| argument of perigee: | 0.5331° |
| revolutions per day: | 13.45446237 |
| mean anomaly at epoch: | 359.5848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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