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 47822U 26145.57013851 +.00000000 +00000-0 +30579-4 0 00002
2 47822 53.1580 257.7128 0001520 89.5336 270.5840 15.31704442 08
| Epoch (UTC): | 25 May 2026 13:40:59 |
| Eccentricity: | 0.0001520 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 257.7128° |
| argument of perigee: | 89.5336° |
| revolutions per day: | 15.31704442 |
| mean anomaly at epoch: | 270.5840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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