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 68156U 26145.29891874 +.00000000 +00000-0 +67194-3 0 00005
2 68156 97.2847 166.8900 0001110 96.1169 264.0201 15.33452189 06
| Epoch (UTC): | 25 May 2026 07:10:26 |
| Eccentricity: | 0.0001110 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.8900° |
| argument of perigee: | 96.1169° |
| revolutions per day: | 15.33452189 |
| mean anomaly at epoch: | 264.0201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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