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 68696U 26145.64000605 +.00000000 +00000-0 +34679-3 0 00009
2 68696 97.6613 221.2649 0016233 139.0139 221.2314 15.09801273 07
| Epoch (UTC): | 25 May 2026 15:21:36 |
| Eccentricity: | 0.0016233 |
| inclination: | 97.6613° |
| perigee height: | 526 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 221.2649° |
| argument of perigee: | 139.0139° |
| revolutions per day: | 15.09801273 |
| mean anomaly at epoch: | 221.2314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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