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 64206U 26145.44505211 +.00000000 +00000-0 +64911-3 0 00005
2 64206 53.1612 43.3399 0001265 98.5913 261.5231 15.30205580 07
| Epoch (UTC): | 25 May 2026 10:40:52 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.3399° |
| argument of perigee: | 98.5913° |
| revolutions per day: | 15.30205580 |
| mean anomaly at epoch: | 261.5231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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