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 68796U 26145.34026250 +.00000000 +00000-0 +27221-3 0 00006
2 68796 97.5038 295.2544 0016656 152.0902 208.1223 15.08203121 05
| Epoch (UTC): | 25 May 2026 08:09:58 |
| Eccentricity: | 0.0016656 |
| inclination: | 97.5038° |
| perigee height: | 530 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 295.2544° |
| argument of perigee: | 152.0902° |
| revolutions per day: | 15.08203121 |
| mean anomaly at epoch: | 208.1223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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