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 68111U 26145.36784499 +.00000000 +00000-0 +80389-3 0 00009
2 68111 97.2833 105.9858 0001506 107.4949 252.6459 15.33456059 07
| Epoch (UTC): | 25 May 2026 08:49:41 |
| Eccentricity: | 0.0001506 |
| inclination: | 97.2833° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 105.9858° |
| argument of perigee: | 107.4949° |
| revolutions per day: | 15.33456059 |
| mean anomaly at epoch: | 252.6459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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