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 47819U 26145.57181911 +.00000000 +00000-0 +22740-4 0 00002
2 47819 53.1589 245.4579 0001545 90.4617 269.6561 15.31702080 02
| Epoch (UTC): | 25 May 2026 13:43:25 |
| Eccentricity: | 0.0001545 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 245.4579° |
| argument of perigee: | 90.4617° |
| revolutions per day: | 15.31702080 |
| mean anomaly at epoch: | 269.6561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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