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 64574U 26145.61778942 +.00000000 +00000-0 +24418-3 0 00003
2 64574 97.7721 260.7588 0003291 70.1025 290.0550 14.95459319 08
| Epoch (UTC): | 25 May 2026 14:49:37 |
| Eccentricity: | 0.0003291 |
| inclination: | 97.7721° |
| perigee height: | 579 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 260.7588° |
| argument of perigee: | 70.1025° |
| revolutions per day: | 14.95459319 |
| mean anomaly at epoch: | 290.0550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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