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 54755U 26145.47707262 +.00000000 +00000-0 +00000-0 0 00002
2 54755 0.0554 344.2624 0006209 94.7140 139.3352 5.00117063 08
| Epoch (UTC): | 25 May 2026 11:26:59 |
| Eccentricity: | 0.0006209 |
| inclination: | 0.0554° |
| perigee height: | 8057 km |
| apogee height: | 8075 km |
| right ascension of ascending node: | 344.2624° |
| argument of perigee: | 94.7140° |
| revolutions per day: | 5.00117063 |
| mean anomaly at epoch: | 139.3352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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