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 58958U 26145.36398324 +.00000000 +00000-0 +40289-4 0 00001
2 58958 39.9890 148.2220 0010695 126.1263 234.0475 13.70485339 04
| Epoch (UTC): | 25 May 2026 08:44:08 |
| Eccentricity: | 0.0010695 |
| inclination: | 39.9890° |
| perigee height: | 990 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 148.2220° |
| argument of perigee: | 126.1263° |
| revolutions per day: | 13.70485339 |
| mean anomaly at epoch: | 234.0475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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