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 53723U 26145.36223863 +.00000000 +00000-0 +18982-4 0 00006
2 53723 53.2145 269.5679 0001247 90.4986 269.6150 15.08832952 08
| Epoch (UTC): | 25 May 2026 08:41:37 |
| Eccentricity: | 0.0001247 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 269.5679° |
| argument of perigee: | 90.4986° |
| revolutions per day: | 15.08832952 |
| mean anomaly at epoch: | 269.6150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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