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 28477U 26070.42160413 +.00000000 +00000-0 +00000-0 0 00007
2 28477 47.4068 139.3525 7023667 92.6168 342.2989 2.23818966 02
| Epoch (UTC): | 11 March 2026 10:07:06 |
| Eccentricity: | 0.7023667 |
| inclination: | 47.4068° |
| perigee height: | 970 km |
| apogee height: | 35648 km |
| right ascension of ascending node: | 139.3525° |
| argument of perigee: | 92.6168° |
| revolutions per day: | 2.23818966 |
| mean anomaly at epoch: | 342.2989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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