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 57249U 26144.80409191 +.00000000 +00000-0 -50125-5 0 00008
2 57249 43.0021 309.7197 0001776 242.8322 117.2349 15.27570245 04
| Epoch (UTC): | 24 May 2026 19:17:53 |
| Eccentricity: | 0.0001776 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.7197° |
| argument of perigee: | 242.8322° |
| revolutions per day: | 15.27570245 |
| mean anomaly at epoch: | 117.2349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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