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 53139U 26145.49844169 +.00000000 +00000-0 -46384-4 0 00007
2 53139 53.2109 189.3117 0000705 113.5016 246.6051 15.08844982 05
| Epoch (UTC): | 25 May 2026 11:57:45 |
| Eccentricity: | 0.0000705 |
| inclination: | 53.2109° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 189.3117° |
| argument of perigee: | 113.5016° |
| revolutions per day: | 15.08844982 |
| mean anomaly at epoch: | 246.6051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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