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 58440U 26145.45663846 +.00000000 +00000-0 +17754-3 0 00001
2 58440 42.9988 131.5876 0001502 273.6176 86.4504 15.27604153 05
| Epoch (UTC): | 25 May 2026 10:57:33 |
| Eccentricity: | 0.0001502 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.5876° |
| argument of perigee: | 273.6176° |
| revolutions per day: | 15.27604153 |
| mean anomaly at epoch: | 86.4504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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