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 57449U 26145.58654125 +.00000000 +00000-0 +84150-4 0 00008
2 57449 43.0036 188.8513 0001694 273.1059 86.9598 15.27581086 06
| Epoch (UTC): | 25 May 2026 14:04:37 |
| Eccentricity: | 0.0001694 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 188.8513° |
| argument of perigee: | 273.1059° |
| revolutions per day: | 15.27581086 |
| mean anomaly at epoch: | 86.9598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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