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 68927U 26144.51258233 +.00000000 +00000-0 -49129-3 0 00000
2 68927 51.8764 181.5941 0002389 136.0910 224.0267 15.36171573 08
| Epoch (UTC): | 24 May 2026 12:18:07 |
| Eccentricity: | 0.0002389 |
| inclination: | 51.8764° |
| perigee height: | 456 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 181.5941° |
| argument of perigee: | 136.0910° |
| revolutions per day: | 15.36171573 |
| mean anomaly at epoch: | 224.0267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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