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 53869U 26145.37511216 +.00000000 +00000-0 +59592-5 0 00003
2 53869 53.2126 289.5337 0001252 96.4864 263.6270 15.08834362 02
| Epoch (UTC): | 25 May 2026 09:00:09 |
| Eccentricity: | 0.0001252 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.5337° |
| argument of perigee: | 96.4864° |
| revolutions per day: | 15.08834362 |
| mean anomaly at epoch: | 263.6270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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