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 64618U 26145.55489227 +.00000000 +00000-0 +43183-3 0 00000
2 64618 53.1580 338.1747 0000598 87.7308 272.3761 15.30212670 02
| Epoch (UTC): | 25 May 2026 13:19:02 |
| Eccentricity: | 0.0000598 |
| inclination: | 53.1580° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.1747° |
| argument of perigee: | 87.7308° |
| revolutions per day: | 15.30212670 |
| mean anomaly at epoch: | 272.3761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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