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 68386U 26145.38468416 +.00000000 +00000-0 +77656-3 0 00006
2 68386 97.2837 288.0167 0001053 76.0308 284.1052 15.33442815 02
| Epoch (UTC): | 25 May 2026 09:13:56 |
| Eccentricity: | 0.0001053 |
| inclination: | 97.2837° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 288.0167° |
| argument of perigee: | 76.0308° |
| revolutions per day: | 15.33442815 |
| mean anomaly at epoch: | 284.1052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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