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 53993U 26145.51174887 +.00000000 +00000-0 -18655-4 0 00001
2 53993 53.2133 224.0058 0001367 94.4718 265.6430 15.08831557 08
| Epoch (UTC): | 25 May 2026 12:16:55 |
| Eccentricity: | 0.0001367 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.0058° |
| argument of perigee: | 94.4718° |
| revolutions per day: | 15.08831557 |
| mean anomaly at epoch: | 265.6430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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