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 47816U 26145.66668980 +.00000000 +00000-0 +88790-3 0 00001
2 47816 53.1587 260.1594 0001267 89.3384 156.5278 15.31697605 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001267 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 260.1594° |
| argument of perigee: | 89.3384° |
| revolutions per day: | 15.31697605 |
| mean anomaly at epoch: | 156.5278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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