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 64915U 26144.84907220 +.00000000 +00000-0 +61268-3 0 00003
2 64915 53.1606 351.9463 0000879 67.2084 292.9010 15.30203136 07
| Epoch (UTC): | 24 May 2026 20:22:39 |
| Eccentricity: | 0.0000879 |
| inclination: | 53.1606° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.9463° |
| argument of perigee: | 67.2084° |
| revolutions per day: | 15.30203136 |
| mean anomaly at epoch: | 292.9010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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