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 35499U 26110.71783010 +.00000000 +00000-0 -42881-4 0 00008
2 35499 82.4858 115.3865 0014549 263.7886 96.1537 12.43007891 05
| Epoch (UTC): | 20 April 2026 17:13:40 |
| Eccentricity: | 0.0014549 |
| inclination: | 82.4858° |
| perigee height: | 1482 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 115.3865° |
| argument of perigee: | 263.7886° |
| revolutions per day: | 12.43007891 |
| mean anomaly at epoch: | 96.1537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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