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 52620U 26144.64926360 +.00000000 +00000-0 -41216-4 0 00000
2 52620 53.2131 303.1215 0001564 93.9921 266.1250 15.08844762 03
| Epoch (UTC): | 24 May 2026 15:34:56 |
| Eccentricity: | 0.0001564 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 303.1215° |
| argument of perigee: | 93.9921° |
| revolutions per day: | 15.08844762 |
| mean anomaly at epoch: | 266.1250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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