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 43820U 26145.59472795 +.00000000 +00000-0 +35214-3 0 00004
2 43820 97.3976 198.4296 0008998 40.1075 320.0824 15.22372511 08
| Epoch (UTC): | 25 May 2026 14:16:24 |
| Eccentricity: | 0.0008998 |
| inclination: | 97.3976° |
| perigee height: | 492 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 198.4296° |
| argument of perigee: | 40.1075° |
| revolutions per day: | 15.22372511 |
| mean anomaly at epoch: | 320.0824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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