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 64901U 26145.54474487 +.00000000 +00000-0 +12708-3 0 00005
2 64901 97.4328 224.5633 0001400 58.5780 301.5592 15.20192111 06
| Epoch (UTC): | 25 May 2026 13:04:25 |
| Eccentricity: | 0.0001400 |
| inclination: | 97.4328° |
| perigee height: | 504 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 224.5633° |
| argument of perigee: | 58.5780° |
| revolutions per day: | 15.20192111 |
| mean anomaly at epoch: | 301.5592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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