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 64207U 26145.41128381 +.00000000 +00000-0 +50695-3 0 00006
2 64207 53.1586 43.1344 0001236 87.0148 273.0994 15.30208668 01
| Epoch (UTC): | 25 May 2026 09:52:14 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.1344° |
| argument of perigee: | 87.0148° |
| revolutions per day: | 15.30208668 |
| mean anomaly at epoch: | 273.0994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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