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 58040U 26145.47529699 +.00000000 +00000-0 -46474-4 0 00009
2 58040 53.1605 171.1986 0001350 87.0547 273.0610 15.34397725 07
| Epoch (UTC): | 25 May 2026 11:24:25 |
| Eccentricity: | 0.0001350 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 171.1986° |
| argument of perigee: | 87.0547° |
| revolutions per day: | 15.34397725 |
| mean anomaly at epoch: | 273.0610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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