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 64599U 26145.24415811 +.00000000 +00000-0 +75406-3 0 00005
2 64599 53.1603 339.7971 0003163 81.6721 278.4638 15.30198849 06
| Epoch (UTC): | 25 May 2026 05:51:35 |
| Eccentricity: | 0.0003163 |
| inclination: | 53.1603° |
| perigee height: | 473 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 339.7971° |
| argument of perigee: | 81.6721° |
| revolutions per day: | 15.30198849 |
| mean anomaly at epoch: | 278.4638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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