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 08458U 26100.19647446 +.00000000 +00000-0 +49139-4 0 00008
2 08458 74.0571 127.2340 0012967 220.7987 139.2195 14.33758230 06
| Epoch (UTC): | 10 April 2026 04:42:55 |
| Eccentricity: | 0.0012967 |
| inclination: | 74.0571° |
| perigee height: | 770 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 127.2340° |
| argument of perigee: | 220.7987° |
| revolutions per day: | 14.33758230 |
| mean anomaly at epoch: | 139.2195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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