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 52290U 26145.32780198 +.00000000 +00000-0 +36934-4 0 00006
2 52290 53.2131 115.0753 0001299 74.2359 285.8776 15.08839998 01
| Epoch (UTC): | 25 May 2026 07:52:02 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.0753° |
| argument of perigee: | 74.2359° |
| revolutions per day: | 15.08839998 |
| mean anomaly at epoch: | 285.8776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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