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 28868U 26145.47439638 +.00000000 +00000-0 +00000-0 0 00007
2 28868 4.2570 76.8562 0004170 354.5657 235.1121 1.00271214 06
| Epoch (UTC): | 25 May 2026 11:23:07 |
| Eccentricity: | 0.0004170 |
| inclination: | 4.2570° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 76.8562° |
| argument of perigee: | 354.5657° |
| revolutions per day: | 1.00271214 |
| mean anomaly at epoch: | 235.1121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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