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 54773U 26145.48094029 +.00000000 +00000-0 +98662-4 0 00008
2 54773 53.2137 59.2667 0002090 66.9452 293.1760 15.08838643 01
| Epoch (UTC): | 25 May 2026 11:32:33 |
| Eccentricity: | 0.0002090 |
| inclination: | 53.2137° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.2667° |
| argument of perigee: | 66.9452° |
| revolutions per day: | 15.08838643 |
| mean anomaly at epoch: | 293.1760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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