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 68417U 26145.63585892 +.00000000 +00000-0 +31861-3 0 00005
2 68417 97.4551 104.5124 0002842 43.7694 316.3766 15.19062896 04
| Epoch (UTC): | 25 May 2026 15:15:38 |
| Eccentricity: | 0.0002842 |
| inclination: | 97.4551° |
| perigee height: | 507 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 104.5124° |
| argument of perigee: | 43.7694° |
| revolutions per day: | 15.19062896 |
| mean anomaly at epoch: | 316.3766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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