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 52196U 26144.91404181 +.00000000 +00000-0 +39920-3 0 00007
2 52196 52.9833 7.7784 0004722 165.0297 195.0849 15.45174250 03
| Epoch (UTC): | 24 May 2026 21:56:13 |
| Eccentricity: | 0.0004722 |
| inclination: | 52.9833° |
| perigee height: | 428 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 7.7784° |
| argument of perigee: | 165.0297° |
| revolutions per day: | 15.45174250 |
| mean anomaly at epoch: | 195.0849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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