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 43799U 26145.59929227 +.00000000 +00000-0 +27209-3 0 00001
2 43799 97.3908 198.9349 0040698 8.0440 352.1443 15.27718535 02
| Epoch (UTC): | 25 May 2026 14:22:58 |
| Eccentricity: | 0.0040698 |
| inclination: | 97.3908° |
| perigee height: | 455 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 198.9349° |
| argument of perigee: | 8.0440° |
| revolutions per day: | 15.27718535 |
| mean anomaly at epoch: | 352.1443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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