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 68299U 26145.35089800 +.00000000 +00000-0 +94010-3 0 00005
2 68299 97.2850 271.6129 0001696 69.8265 290.3183 15.75245427 01
| Epoch (UTC): | 25 May 2026 08:25:17 |
| Eccentricity: | 0.0001696 |
| inclination: | 97.2850° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6129° |
| argument of perigee: | 69.8265° |
| revolutions per day: | 15.75245427 |
| mean anomaly at epoch: | 290.3183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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