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 30406U 26017.63292101 +.00000000 +00000-0 +10501-2 0 00005
2 30406 98.6213 269.0440 0280211 266.7584 119.1880 13.59361554 01
| Epoch (UTC): | 17 January 2026 15:11:24 |
| Eccentricity: | 0.0280211 |
| inclination: | 98.6213° |
| perigee height: | 830 km |
| apogee height: | 1246 km |
| right ascension of ascending node: | 269.0440° |
| argument of perigee: | 266.7584° |
| revolutions per day: | 13.59361554 |
| mean anomaly at epoch: | 119.1880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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