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 53015U 26145.26015957 +.00000000 +00000-0 -71055-4 0 00003
2 53015 53.2138 100.3808 0001331 84.5363 275.5781 15.08836048 03
| Epoch (UTC): | 25 May 2026 06:14:37 |
| Eccentricity: | 0.0001331 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.3808° |
| argument of perigee: | 84.5363° |
| revolutions per day: | 15.08836048 |
| mean anomaly at epoch: | 275.5781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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