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 57243U 26145.48879679 +.00000000 +00000-0 +13120-4 0 00001
2 57243 43.0033 306.3245 0001210 272.4789 87.5925 15.27577649 01
| Epoch (UTC): | 25 May 2026 11:43:52 |
| Eccentricity: | 0.0001210 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.3245° |
| argument of perigee: | 272.4789° |
| revolutions per day: | 15.27577649 |
| mean anomaly at epoch: | 87.5925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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