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 68637U 26144.77265250 +.00000000 +00000-0 +41659-4 0 00003
2 68637 88.9877 323.4337 0011458 69.0309 291.2074 13.62578006 03
| Epoch (UTC): | 24 May 2026 18:32:37 |
| Eccentricity: | 0.0011458 |
| inclination: | 88.9877° |
| perigee height: | 1018 km |
| apogee height: | 1035 km |
| right ascension of ascending node: | 323.4337° |
| argument of perigee: | 69.0309° |
| revolutions per day: | 13.62578006 |
| mean anomaly at epoch: | 291.2074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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