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 57630U 26145.64403388 +.00000000 +00000-0 +20299-3 0 00003
2 57630 45.0028 39.0844 0006941 142.9591 217.1748 14.63809840 04
| Epoch (UTC): | 25 May 2026 15:27:24 |
| Eccentricity: | 0.0006941 |
| inclination: | 45.0028° |
| perigee height: | 676 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 39.0844° |
| argument of perigee: | 142.9591° |
| revolutions per day: | 14.63809840 |
| mean anomaly at epoch: | 217.1748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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