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 28786U 26145.60745279 +.00000000 +00000-0 +00000-0 0 00002
2 28786 0.1887 86.1658 0002002 333.7744 161.4328 1.00271457 08
| Epoch (UTC): | 25 May 2026 14:34:43 |
| Eccentricity: | 0.0002002 |
| inclination: | 0.1887° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 86.1658° |
| argument of perigee: | 333.7744° |
| revolutions per day: | 1.00271457 |
| mean anomaly at epoch: | 161.4328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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