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 52502U 26145.15940856 +.00000000 +00000-0 +67079-4 0 00006
2 52502 53.2143 55.8608 0001714 62.7244 297.3923 15.08839491 07
| Epoch (UTC): | 25 May 2026 03:49:32 |
| Eccentricity: | 0.0001714 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 55.8608° |
| argument of perigee: | 62.7244° |
| revolutions per day: | 15.08839491 |
| mean anomaly at epoch: | 297.3923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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