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 57914U 26145.61365726 +.00000000 +00000-0 +27027-4 0 00005
2 57914 43.0035 105.2034 0001396 296.2031 63.8678 15.27577499 04
| Epoch (UTC): | 25 May 2026 14:43:39 |
| Eccentricity: | 0.0001396 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 105.2034° |
| argument of perigee: | 296.2031° |
| revolutions per day: | 15.27577499 |
| mean anomaly at epoch: | 63.8678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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