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 58955U 26145.34134601 +.00000000 +00000-0 +78851-4 0 00008
2 58955 39.9892 148.8585 0018724 109.5110 250.7661 13.70466177 01
| Epoch (UTC): | 25 May 2026 08:11:32 |
| Eccentricity: | 0.0018724 |
| inclination: | 39.9892° |
| perigee height: | 984 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 148.8585° |
| argument of perigee: | 109.5110° |
| revolutions per day: | 13.70466177 |
| mean anomaly at epoch: | 250.7661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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