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 62982U 26145.37039012 +.00000000 +00000-0 +17484-2 0 00009
2 62982 43.0012 259.1325 0001891 246.4281 113.6388 15.70975522 05
| Epoch (UTC): | 25 May 2026 08:53:21 |
| Eccentricity: | 0.0001891 |
| inclination: | 43.0012° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 259.1325° |
| argument of perigee: | 246.4281° |
| revolutions per day: | 15.70975522 |
| mean anomaly at epoch: | 113.6388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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