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 00659U 26104.60331434 +.00000000 +00000-0 +50549-3 0 00006
2 00659 67.1597 223.3384 0588840 328.0278 48.6458 12.66813626 01
| Epoch (UTC): | 14 April 2026 14:28:46 |
| Eccentricity: | 0.0588840 |
| inclination: | 67.1597° |
| perigee height: | 937 km |
| apogee height: | 1853 km |
| right ascension of ascending node: | 223.3384° |
| argument of perigee: | 328.0278° |
| revolutions per day: | 12.66813626 |
| mean anomaly at epoch: | 48.6458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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