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 64203U 26145.41445067 +.00000000 +00000-0 +51527-3 0 00000
2 64203 53.1575 43.1529 0001051 77.6716 282.4403 15.30205150 03
| Epoch (UTC): | 25 May 2026 09:56:48 |
| Eccentricity: | 0.0001051 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.1529° |
| argument of perigee: | 77.6716° |
| revolutions per day: | 15.30205150 |
| mean anomaly at epoch: | 282.4403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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