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 52094U 26145.18425153 +.00000000 +00000-0 +59974-4 0 00008
2 52094 53.2119 105.7238 0001524 89.4796 270.6370 15.08832848 06
| Epoch (UTC): | 25 May 2026 04:25:19 |
| Eccentricity: | 0.0001524 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.7238° |
| argument of perigee: | 89.4796° |
| revolutions per day: | 15.08832848 |
| mean anomaly at epoch: | 270.6370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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