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 54011U 26145.41472303 +.00000000 +00000-0 +46029-4 0 00001
2 54011 53.2113 219.8392 0001034 78.3200 281.7908 15.08840099 09
| Epoch (UTC): | 25 May 2026 09:57:12 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 219.8392° |
| argument of perigee: | 78.3200° |
| revolutions per day: | 15.08840099 |
| mean anomaly at epoch: | 281.7908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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