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 59219U 26145.30033449 +.00000000 +00000-0 +17644-4 0 00009
2 59219 53.1599 158.4518 0001111 86.6042 273.5087 15.34387462 07
| Epoch (UTC): | 25 May 2026 07:12:28 |
| Eccentricity: | 0.0001111 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 158.4518° |
| argument of perigee: | 86.6042° |
| revolutions per day: | 15.34387462 |
| mean anomaly at epoch: | 273.5087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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