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 64577U 26145.56288941 +.00000000 +00000-0 +20181-3 0 00008
2 64577 97.7716 251.4864 0021988 58.1246 302.2099 14.74406619 09
| Epoch (UTC): | 25 May 2026 13:30:33 |
| Eccentricity: | 0.0021988 |
| inclination: | 97.7716° |
| perigee height: | 632 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 251.4864° |
| argument of perigee: | 58.1246° |
| revolutions per day: | 14.74406619 |
| mean anomaly at epoch: | 302.2099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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