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 57258U 26145.46438119 +.00000000 +00000-0 +40409-4 0 00005
2 57258 43.0022 306.1278 0001320 261.8210 98.2492 15.27576179 07
| Epoch (UTC): | 25 May 2026 11:08:42 |
| Eccentricity: | 0.0001320 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.1278° |
| argument of perigee: | 261.8210° |
| revolutions per day: | 15.27576179 |
| mean anomaly at epoch: | 98.2492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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