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 68810U 26145.55942041 +.00000000 +00000-0 +13097-2 0 00006
2 68810 97.2846 352.2275 0001213 96.7691 263.3712 15.75248762 03
| Epoch (UTC): | 25 May 2026 13:25:33 |
| Eccentricity: | 0.0001213 |
| inclination: | 97.2846° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2275° |
| argument of perigee: | 96.7691° |
| revolutions per day: | 15.75248762 |
| mean anomaly at epoch: | 263.3712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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