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 62633U 26145.15626881 +.00000000 +00000-0 +36476-3 0 00007
2 62633 97.4015 227.2605 0003935 50.2670 309.8916 15.28867786 06
| Epoch (UTC): | 25 May 2026 03:45:01 |
| Eccentricity: | 0.0003935 |
| inclination: | 97.4015° |
| perigee height: | 476 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 227.2605° |
| argument of perigee: | 50.2670° |
| revolutions per day: | 15.28867786 |
| mean anomaly at epoch: | 309.8916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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