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 62229U 26145.54340074 +.00000000 +00000-0 +12834-2 0 00009
2 62229 53.1578 82.2999 0001242 81.5771 278.5388 15.69769763 09
| Epoch (UTC): | 25 May 2026 13:02:29 |
| Eccentricity: | 0.0001242 |
| inclination: | 53.1578° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 82.2999° |
| argument of perigee: | 81.5771° |
| revolutions per day: | 15.69769763 |
| mean anomaly at epoch: | 278.5388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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