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 64797U 26145.43600613 +.00000000 +00000-0 +45630-3 0 00008
2 64797 70.0005 300.9090 0003125 267.3281 92.7520 14.98339420 06
| Epoch (UTC): | 25 May 2026 10:27:50 |
| Eccentricity: | 0.0003125 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.9090° |
| argument of perigee: | 267.3281° |
| revolutions per day: | 14.98339420 |
| mean anomaly at epoch: | 92.7520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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