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 52611U 26145.12030855 +.00000000 +00000-0 +96701-6 0 00009
2 52611 53.2145 301.0079 0001387 87.3930 272.7221 15.08835333 08
| Epoch (UTC): | 25 May 2026 02:53:14 |
| Eccentricity: | 0.0001387 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 301.0079° |
| argument of perigee: | 87.3930° |
| revolutions per day: | 15.08835333 |
| mean anomaly at epoch: | 272.7221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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