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 53439U 26145.63828806 +.00000000 +00000-0 +83617-4 0 00005
2 53439 53.2130 118.4506 0001221 78.1373 281.9756 15.08827304 06
| Epoch (UTC): | 25 May 2026 15:19:08 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 118.4506° |
| argument of perigee: | 78.1373° |
| revolutions per day: | 15.08827304 |
| mean anomaly at epoch: | 281.9756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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