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 64221U 26145.42183693 +.00000000 +00000-0 +33428-3 0 00005
2 64221 53.1597 43.1951 0001504 86.0211 274.0962 15.30208647 04
| Epoch (UTC): | 25 May 2026 10:07:26 |
| Eccentricity: | 0.0001504 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.1951° |
| argument of perigee: | 86.0211° |
| revolutions per day: | 15.30208647 |
| mean anomaly at epoch: | 274.0962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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