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 68868U 26144.99230991 +.00000000 +00000-0 +72759-3 0 00001
2 68868 51.8849 354.3395 0001431 219.6202 140.4681 15.38744475 08
| Epoch (UTC): | 24 May 2026 23:48:55 |
| Eccentricity: | 0.0001431 |
| inclination: | 51.8849° |
| perigee height: | 449 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 354.3395° |
| argument of perigee: | 219.6202° |
| revolutions per day: | 15.38744475 |
| mean anomaly at epoch: | 140.4681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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