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 52643U 26145.35356397 +.00000000 +00000-0 +39360-4 0 00007
2 52643 53.2137 274.9337 0001179 95.0879 265.0248 15.08836543 04
| Epoch (UTC): | 25 May 2026 08:29:07 |
| Eccentricity: | 0.0001179 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 274.9337° |
| argument of perigee: | 95.0879° |
| revolutions per day: | 15.08836543 |
| mean anomaly at epoch: | 265.0248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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