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 54649U 26145.57369427 +.00000000 +00000-0 -56000-4 0 00008
2 54649 87.9252 248.4735 0002421 96.6982 263.4427 13.21825194 09
| Epoch (UTC): | 25 May 2026 13:46:07 |
| Eccentricity: | 0.0002421 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 248.4735° |
| argument of perigee: | 96.6982° |
| revolutions per day: | 13.21825194 |
| mean anomaly at epoch: | 263.4427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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