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 68122U 26145.33793480 +.00000000 +00000-0 +96854-3 0 00002
2 68122 97.2847 106.0276 0000651 87.2772 272.8545 15.33463853 09
| Epoch (UTC): | 25 May 2026 08:06:37 |
| Eccentricity: | 0.0000651 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 106.0276° |
| argument of perigee: | 87.2772° |
| revolutions per day: | 15.33463853 |
| mean anomaly at epoch: | 272.8545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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