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 53438U 26145.22882367 +.00000000 +00000-0 -66776-4 0 00009
2 53438 53.2140 120.1652 0001259 73.9894 286.1237 15.08849591 03
| Epoch (UTC): | 25 May 2026 05:29:30 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.1652° |
| argument of perigee: | 73.9894° |
| revolutions per day: | 15.08849591 |
| mean anomaly at epoch: | 286.1237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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