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 52352U 26145.45748490 +.00000000 +00000-0 +65540-4 0 00003
2 52352 53.2145 214.4970 0001150 89.9507 270.1617 15.08840144 00
| Epoch (UTC): | 25 May 2026 10:58:46 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.4970° |
| argument of perigee: | 89.9507° |
| revolutions per day: | 15.08840144 |
| mean anomaly at epoch: | 270.1617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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