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 64897U 26145.63437244 +.00000000 +00000-0 +56683-3 0 00009
2 64897 97.6709 210.5021 0004415 351.5881 8.5265 14.96346202 03
| Epoch (UTC): | 25 May 2026 15:13:29 |
| Eccentricity: | 0.0004415 |
| inclination: | 97.6709° |
| perigee height: | 575 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 210.5021° |
| argument of perigee: | 351.5881° |
| revolutions per day: | 14.96346202 |
| mean anomaly at epoch: | 8.5265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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