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 53032U 26145.28958523 +.00000000 +00000-0 +90855-5 0 00008
2 53032 53.2137 100.2490 0001319 72.7955 287.3182 15.08839084 08
| Epoch (UTC): | 25 May 2026 06:57:00 |
| Eccentricity: | 0.0001319 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.2490° |
| argument of perigee: | 72.7955° |
| revolutions per day: | 15.08839084 |
| mean anomaly at epoch: | 287.3182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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