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 64034U 26145.40256382 +.00000000 +00000-0 +51756-3 0 00005
2 64034 69.9999 281.0090 0003165 268.0934 91.9863 14.98334434 06
| Epoch (UTC): | 25 May 2026 09:39:41 |
| Eccentricity: | 0.0003165 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.0090° |
| argument of perigee: | 268.0934° |
| revolutions per day: | 14.98334434 |
| mean anomaly at epoch: | 91.9863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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