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 53024U 26145.30430822 +.00000000 +00000-0 -12719-3 0 00001
2 53024 53.2128 100.1830 0001276 87.3790 272.7349 15.08858909 07
| Epoch (UTC): | 25 May 2026 07:18:12 |
| Eccentricity: | 0.0001276 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.1830° |
| argument of perigee: | 87.3790° |
| revolutions per day: | 15.08858909 |
| mean anomaly at epoch: | 272.7349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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