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 47368U 26145.47154605 +.00000000 +00000-0 +10932-3 0 00009
2 47368 53.1591 65.3922 0001267 86.7789 273.3357 15.31701357 05
| Epoch (UTC): | 25 May 2026 11:19:01 |
| Eccentricity: | 0.0001267 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 65.3922° |
| argument of perigee: | 86.7789° |
| revolutions per day: | 15.31701357 |
| mean anomaly at epoch: | 273.3357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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