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 64913U 26145.27042250 +.00000000 +00000-0 +98379-3 0 00005
2 64913 53.1590 349.6020 0001363 68.8108 291.3038 15.31721856 01
| Epoch (UTC): | 25 May 2026 06:29:24 |
| Eccentricity: | 0.0001363 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 349.6020° |
| argument of perigee: | 68.8108° |
| revolutions per day: | 15.31721856 |
| mean anomaly at epoch: | 291.3038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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