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 68105U 26145.38144126 +.00000000 +00000-0 +82848-3 0 00003
2 68105 97.2824 105.9646 0001892 105.4996 254.6456 15.33453718 01
| Epoch (UTC): | 25 May 2026 09:09:16 |
| Eccentricity: | 0.0001892 |
| inclination: | 97.2824° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 105.9646° |
| argument of perigee: | 105.4996° |
| revolutions per day: | 15.33453718 |
| mean anomaly at epoch: | 254.6456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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