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 55921U 26145.63199255 +.00000000 +00000-0 +13736-3 0 00006
2 55921 69.9993 110.4083 0003321 253.3558 106.7237 14.98322203 06
| Epoch (UTC): | 25 May 2026 15:10:04 |
| Eccentricity: | 0.0003321 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 110.4083° |
| argument of perigee: | 253.3558° |
| revolutions per day: | 14.98322203 |
| mean anomaly at epoch: | 106.7237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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