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 64921U 26145.58335647 +.00000000 +00000-0 +78854-3 0 00009
2 64921 53.1605 348.5867 0001209 100.9015 321.5637 15.33536683 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001209 |
| inclination: | 53.1605° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 348.5867° |
| argument of perigee: | 100.9015° |
| revolutions per day: | 15.33536683 |
| mean anomaly at epoch: | 321.5637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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