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 68612U 26145.58335647 +.00000000 +00000-0 +93590-3 0 00004
2 68612 97.2846 345.1095 0001198 104.2667 74.6208 15.49184179 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001198 |
| inclination: | 97.2846° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 345.1095° |
| argument of perigee: | 104.2667° |
| revolutions per day: | 15.49184179 |
| mean anomaly at epoch: | 74.6208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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