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 53868U 26145.39445713 +.00000000 +00000-0 +49234-5 0 00004
2 53868 53.2157 279.6851 0001246 90.8522 269.2613 15.08835736 07
| Epoch (UTC): | 25 May 2026 09:28:01 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.2157° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 279.6851° |
| argument of perigee: | 90.8522° |
| revolutions per day: | 15.08835736 |
| mean anomaly at epoch: | 269.2613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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