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 53887U 26145.53248366 +.00000000 +00000-0 +22852-4 0 00002
2 53887 53.2126 339.2690 0001304 91.0951 269.0190 15.08838032 02
| Epoch (UTC): | 25 May 2026 12:46:46 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 339.2690° |
| argument of perigee: | 91.0951° |
| revolutions per day: | 15.08838032 |
| mean anomaly at epoch: | 269.0190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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