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 53860U 26145.15344251 +.00000000 +00000-0 +50954-4 0 00005
2 53860 53.2135 300.9764 0001094 86.1673 273.9445 15.08839307 05
| Epoch (UTC): | 25 May 2026 03:40:57 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 300.9764° |
| argument of perigee: | 86.1673° |
| revolutions per day: | 15.08839307 |
| mean anomaly at epoch: | 273.9445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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