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 68610U 26145.58335647 +.00000000 +00000-0 -22211-1 0 00003
2 68610 97.2844 345.1110 0002270 69.6274 115.3198 15.64363864 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002270 |
| inclination: | 97.2844° |
| perigee height: | 374 km |
| apogee height: | 377 km |
| right ascension of ascending node: | 345.1110° |
| argument of perigee: | 69.6274° |
| revolutions per day: | 15.64363864 |
| mean anomaly at epoch: | 115.3198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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