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 28359U 26066.25046867 +.00000000 +00000-0 +96280-3 0 00006
2 28359 49.5291 26.6138 4500829 126.4938 283.9819 6.50571445 03
| Epoch (UTC): | 07 March 2026 06:00:40 |
| Eccentricity: | 0.4500829 |
| inclination: | 49.5291° |
| perigee height: | 287 km |
| apogee height: | 11198 km |
| right ascension of ascending node: | 26.6138° |
| argument of perigee: | 126.4938° |
| revolutions per day: | 6.50571445 |
| mean anomaly at epoch: | 283.9819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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