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 53850U 26145.17454323 +.00000000 +00000-0 +34824-4 0 00006
2 53850 53.2148 310.3835 0001263 86.3952 273.7185 15.08837554 03
| Epoch (UTC): | 25 May 2026 04:11:20 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 310.3835° |
| argument of perigee: | 86.3952° |
| revolutions per day: | 15.08837554 |
| mean anomaly at epoch: | 273.7185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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