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 43530U 26145.63849280 +.00000000 +00000-0 +13745-3 0 00009
2 43530 97.7824 214.1323 0001865 86.7977 273.3450 14.81948413 01
| Epoch (UTC): | 25 May 2026 15:19:25 |
| Eccentricity: | 0.0001865 |
| inclination: | 97.7824° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 214.1323° |
| argument of perigee: | 86.7977° |
| revolutions per day: | 14.81948413 |
| mean anomaly at epoch: | 273.3450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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