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 68114U 26145.62342855 +.00000000 +00000-0 +64423-3 0 00008
2 68114 97.2850 106.2513 0001417 97.8689 262.2715 15.33451659 08
| Epoch (UTC): | 25 May 2026 14:57:44 |
| Eccentricity: | 0.0001417 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 106.2513° |
| argument of perigee: | 97.8689° |
| revolutions per day: | 15.33451659 |
| mean anomaly at epoch: | 262.2715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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