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 57508U 26145.45459700 +.00000000 +00000-0 +10814-3 0 00007
2 57508 43.0029 302.6845 0001399 265.8246 94.2446 15.27586559 00
| Epoch (UTC): | 25 May 2026 10:54:37 |
| Eccentricity: | 0.0001399 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.6845° |
| argument of perigee: | 265.8246° |
| revolutions per day: | 15.27586559 |
| mean anomaly at epoch: | 94.2446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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