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 28628U 26145.26735265 +.00000000 +00000-0 +00000-0 0 00003
2 28628 5.1391 42.7255 0002823 19.4843 94.9865 1.00271835 04
| Epoch (UTC): | 25 May 2026 06:24:59 |
| Eccentricity: | 0.0002823 |
| inclination: | 5.1391° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 42.7255° |
| argument of perigee: | 19.4843° |
| revolutions per day: | 1.00271835 |
| mean anomaly at epoch: | 94.9865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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