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 47854U 26145.63908332 +.00000000 +00000-0 +33690-4 0 00008
2 47854 63.4068 315.9366 0173036 0.4566 359.6588 13.45445946 00
| Epoch (UTC): | 25 May 2026 15:20:16 |
| Eccentricity: | 0.0173036 |
| inclination: | 63.4068° |
| perigee height: | 960 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 315.9366° |
| argument of perigee: | 0.4566° |
| revolutions per day: | 13.45445946 |
| mean anomaly at epoch: | 359.6588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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