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 68872U 26145.55709131 +.00000000 +00000-0 +63571-3 0 00008
2 68872 51.8722 352.0928 0010530 218.4205 141.6032 15.35635376 09
| Epoch (UTC): | 25 May 2026 13:22:12 |
| Eccentricity: | 0.0010530 |
| inclination: | 51.8722° |
| perigee height: | 452 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 352.0928° |
| argument of perigee: | 218.4205° |
| revolutions per day: | 15.35635376 |
| mean anomaly at epoch: | 141.6032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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