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 64570U 26145.59454513 +.00000000 +00000-0 +29129-3 0 00005
2 64570 97.7693 260.2439 0003061 59.0753 301.0768 14.94392206 05
| Epoch (UTC): | 25 May 2026 14:16:08 |
| Eccentricity: | 0.0003061 |
| inclination: | 97.7693° |
| perigee height: | 582 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 260.2439° |
| argument of perigee: | 59.0753° |
| revolutions per day: | 14.94392206 |
| mean anomaly at epoch: | 301.0768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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