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 68874U 26145.55186094 +.00000000 +00000-0 +64316-3 0 00005
2 68874 51.8750 352.0632 0008614 213.7642 146.2797 15.36108712 06
| Epoch (UTC): | 25 May 2026 13:14:40 |
| Eccentricity: | 0.0008614 |
| inclination: | 51.8750° |
| perigee height: | 452 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 352.0632° |
| argument of perigee: | 213.7642° |
| revolutions per day: | 15.36108712 |
| mean anomaly at epoch: | 146.2797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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