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 52602U 26145.43540779 +.00000000 +00000-0 -77817-4 0 00000
2 52602 53.2137 294.5929 0001183 109.2477 250.8644 15.08843195 04
| Epoch (UTC): | 25 May 2026 10:26:59 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.5929° |
| argument of perigee: | 109.2477° |
| revolutions per day: | 15.08843195 |
| mean anomaly at epoch: | 250.8644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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