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 36799U 26110.58585481 +.00000000 +00000-0 +58523-3 0 00007
2 36799 98.0697 52.1441 0004612 89.2923 270.8843 15.29483302 07
| Epoch (UTC): | 20 April 2026 14:03:37 |
| Eccentricity: | 0.0004612 |
| inclination: | 98.0697° |
| perigee height: | 474 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 52.1441° |
| argument of perigee: | 89.2923° |
| revolutions per day: | 15.29483302 |
| mean anomaly at epoch: | 270.8843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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