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 53159U 26145.48095072 +.00000000 +00000-0 +29979-4 0 00009
2 53159 53.2132 179.3879 0001427 63.3242 296.7897 15.08836958 00
| Epoch (UTC): | 25 May 2026 11:32:34 |
| Eccentricity: | 0.0001427 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.3879° |
| argument of perigee: | 63.3242° |
| revolutions per day: | 15.08836958 |
| mean anomaly at epoch: | 296.7897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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