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 68951U 26145.58335647 +.00000000 +00000-0 -22390-1 0 00009
2 68951 53.1593 268.0895 0000934 65.1509 29.5511 15.64418611 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000934 |
| inclination: | 53.1593° |
| perigee height: | 374 km |
| apogee height: | 376 km |
| right ascension of ascending node: | 268.0895° |
| argument of perigee: | 65.1509° |
| revolutions per day: | 15.64418611 |
| mean anomaly at epoch: | 29.5511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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