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 62234U 26145.20745808 +.00000000 +00000-0 +46363-3 0 00007
2 62234 53.1586 224.2039 0001121 100.3332 259.7795 15.30207012 01
| Epoch (UTC): | 25 May 2026 04:58:44 |
| Eccentricity: | 0.0001121 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 224.2039° |
| argument of perigee: | 100.3332° |
| revolutions per day: | 15.30207012 |
| mean anomaly at epoch: | 259.7795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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