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 57811U 26145.41966758 +.00000000 +00000-0 -55306-4 0 00003
2 57811 43.0036 160.8131 0001077 273.4149 86.6579 15.27567157 02
| Epoch (UTC): | 25 May 2026 10:04:19 |
| Eccentricity: | 0.0001077 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.8131° |
| argument of perigee: | 273.4149° |
| revolutions per day: | 15.27567157 |
| mean anomaly at epoch: | 86.6579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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