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 68812U 26145.55871402 +.00000000 +00000-0 +13094-2 0 00007
2 68812 97.2839 352.2281 0001532 92.3911 267.7529 15.75257219 06
| Epoch (UTC): | 25 May 2026 13:24:32 |
| Eccentricity: | 0.0001532 |
| inclination: | 97.2839° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2281° |
| argument of perigee: | 92.3911° |
| revolutions per day: | 15.75257219 |
| mean anomaly at epoch: | 267.7529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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