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 64791U 26145.42764946 +.00000000 +00000-0 +27300-3 0 00005
2 64791 70.0004 300.8808 0003111 265.4343 94.6461 14.98335406 03
| Epoch (UTC): | 25 May 2026 10:15:48 |
| Eccentricity: | 0.0003111 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8808° |
| argument of perigee: | 265.4343° |
| revolutions per day: | 14.98335406 |
| mean anomaly at epoch: | 94.6461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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