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 57472U 26145.62623645 +.00000000 +00000-0 +98672-4 0 00006
2 57472 43.0008 261.5965 0001071 272.3083 87.7646 15.27590759 08
| Epoch (UTC): | 25 May 2026 15:01:46 |
| Eccentricity: | 0.0001071 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 261.5965° |
| argument of perigee: | 272.3083° |
| revolutions per day: | 15.27590759 |
| mean anomaly at epoch: | 87.7646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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