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 64875U 26145.62761418 +.00000000 +00000-0 +70089-3 0 00003
2 64875 97.4046 213.9617 0001913 124.8017 235.3405 15.31625861 08
| Epoch (UTC): | 25 May 2026 15:03:45 |
| Eccentricity: | 0.0001913 |
| inclination: | 97.4046° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 213.9617° |
| argument of perigee: | 124.8017° |
| revolutions per day: | 15.31625861 |
| mean anomaly at epoch: | 235.3405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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