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 62063U 26145.04632638 +.00000000 +00000-0 +11018-2 0 00003
2 62063 53.1571 55.0318 0000855 72.4875 287.6236 15.69770123 09
| Epoch (UTC): | 25 May 2026 01:06:42 |
| Eccentricity: | 0.0000855 |
| inclination: | 53.1571° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 55.0318° |
| argument of perigee: | 72.4875° |
| revolutions per day: | 15.69770123 |
| mean anomaly at epoch: | 287.6236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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