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 63212U 26145.47360375 +.00000000 +00000-0 +84021-3 0 00008
2 63212 97.3857 46.5459 0003830 124.2037 235.9578 15.50581699 09
| Epoch (UTC): | 25 May 2026 11:21:59 |
| Eccentricity: | 0.0003830 |
| inclination: | 97.3857° |
| perigee height: | 412 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 46.5459° |
| argument of perigee: | 124.2037° |
| revolutions per day: | 15.50581699 |
| mean anomaly at epoch: | 235.9578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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