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 43058U 26144.11116971 +.00000000 +00000-0 +00000-0 0 00007
2 43058 55.0782 222.1648 0004251 273.8100 86.1948 1.70474790 02
| Epoch (UTC): | 24 May 2026 02:40:05 |
| Eccentricity: | 0.0004251 |
| inclination: | 55.0782° |
| perigee height: | 23210 km |
| apogee height: | 23235 km |
| right ascension of ascending node: | 222.1648° |
| argument of perigee: | 273.8100° |
| revolutions per day: | 1.70474790 |
| mean anomaly at epoch: | 86.1948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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