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 53932U 26145.45932245 +.00000000 +00000-0 +12544-3 0 00006
2 53932 53.2149 314.5802 0000964 100.2217 259.8884 15.08852039 08
| Epoch (UTC): | 25 May 2026 11:01:25 |
| Eccentricity: | 0.0000964 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 314.5802° |
| argument of perigee: | 100.2217° |
| revolutions per day: | 15.08852039 |
| mean anomaly at epoch: | 259.8884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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