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 64205U 26145.50003470 +.00000000 +00000-0 -95937-3 0 00004
2 64205 53.1609 43.0124 0000968 82.3686 257.1004 15.34394626 05
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0000968 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 43.0124° |
| argument of perigee: | 82.3686° |
| revolutions per day: | 15.34394626 |
| mean anomaly at epoch: | 257.1004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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