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 62160U 26145.17158039 +.00000000 +00000-0 +88809-3 0 00006
2 62160 43.0020 86.4527 0001299 283.0538 77.0168 15.27604076 05
| Epoch (UTC): | 25 May 2026 04:07:04 |
| Eccentricity: | 0.0001299 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 86.4527° |
| argument of perigee: | 283.0538° |
| revolutions per day: | 15.27604076 |
| mean anomaly at epoch: | 77.0168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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