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 35500U 26145.50306208 +.00000000 +00000-0 +26853-3 0 00005
2 35500 82.4865 101.9957 0005923 208.5329 151.5427 12.41519383 00
| Epoch (UTC): | 25 May 2026 12:04:24 |
| Eccentricity: | 0.0005923 |
| inclination: | 82.4865° |
| perigee height: | 1496 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 101.9957° |
| argument of perigee: | 208.5329° |
| revolutions per day: | 12.41519383 |
| mean anomaly at epoch: | 151.5427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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