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 68199U 26145.77709235 +.00000000 +00000-0 +24626-3 0 00007
2 68199 97.5332 220.9067 0013166 33.8024 326.4043 15.10622897 00
| Epoch (UTC): | 25 May 2026 18:39:00 |
| Eccentricity: | 0.0013166 |
| inclination: | 97.5332° |
| perigee height: | 525 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 220.9067° |
| argument of perigee: | 33.8024° |
| revolutions per day: | 15.10622897 |
| mean anomaly at epoch: | 326.4043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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