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 28446U 26145.47485117 +.00000000 +00000-0 +00000-0 0 00002
2 28446 0.0234 309.2455 0002334 122.5204 237.1817 1.00272381 04
| Epoch (UTC): | 25 May 2026 11:23:47 |
| Eccentricity: | 0.0002334 |
| inclination: | 0.0234° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 309.2455° |
| argument of perigee: | 122.5204° |
| revolutions per day: | 1.00272381 |
| mean anomaly at epoch: | 237.1817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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