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 53012U 26145.22242895 +.00000000 +00000-0 +68852-4 0 00009
2 53012 53.2135 110.5508 0001376 75.5616 284.5528 15.08839050 02
| Epoch (UTC): | 25 May 2026 05:20:17 |
| Eccentricity: | 0.0001376 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.5508° |
| argument of perigee: | 75.5616° |
| revolutions per day: | 15.08839050 |
| mean anomaly at epoch: | 284.5528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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