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 58098U 26145.44160998 +.00000000 +00000-0 +26969-4 0 00008
2 58098 53.1588 168.9591 0001142 91.9830 268.1301 15.30190996 03
| Epoch (UTC): | 25 May 2026 10:35:55 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9591° |
| argument of perigee: | 91.9830° |
| revolutions per day: | 15.30190996 |
| mean anomaly at epoch: | 268.1301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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