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 57248U 26145.45410741 +.00000000 +00000-0 +19412-4 0 00004
2 57248 43.0025 306.0570 0001627 272.2705 87.7961 15.27573338 06
| Epoch (UTC): | 25 May 2026 10:53:54 |
| Eccentricity: | 0.0001627 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.0570° |
| argument of perigee: | 272.2705° |
| revolutions per day: | 15.27573338 |
| mean anomaly at epoch: | 87.7961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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