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 52501U 26145.49702612 +.00000000 +00000-0 +90513-4 0 00007
2 52501 53.2145 64.1161 0001231 85.5659 274.5474 15.08833941 04
| Epoch (UTC): | 25 May 2026 11:55:43 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.1161° |
| argument of perigee: | 85.5659° |
| revolutions per day: | 15.08833941 |
| mean anomaly at epoch: | 274.5474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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