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 68891U 26145.57651955 +.00000000 +00000-0 +72444-3 0 00000
2 68891 51.8863 351.5017 0000487 144.3480 215.7539 15.38166491 06
| Epoch (UTC): | 25 May 2026 13:50:11 |
| Eccentricity: | 0.0000487 |
| inclination: | 51.8863° |
| perigee height: | 451 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 351.5017° |
| argument of perigee: | 144.3480° |
| revolutions per day: | 15.38166491 |
| mean anomaly at epoch: | 215.7539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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