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 43162U 26146.12259397 +.00000000 +00000-0 +00000-0 0 00006
2 43162 2.1697 11.0895 0002246 45.0957 72.2441 1.00272524 04
| Epoch (UTC): | 26 May 2026 02:56:32 |
| Eccentricity: | 0.0002246 |
| inclination: | 2.1697° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 11.0895° |
| argument of perigee: | 45.0957° |
| revolutions per day: | 1.00272524 |
| mean anomaly at epoch: | 72.2441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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