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 68834U 26131.61679669 +.00000000 +00000-0 +12871-3 0 00007
2 68834 55.0023 181.4507 0009842 9.4049 350.7153 15.19483940 09
| Epoch (UTC): | 11 May 2026 14:48:11 |
| Eccentricity: | 0.0009842 |
| inclination: | 55.0023° |
| perigee height: | 501 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 181.4507° |
| argument of perigee: | 9.4049° |
| revolutions per day: | 15.19483940 |
| mean anomaly at epoch: | 350.7153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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