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 28414U 26018.00498097 +.00000000 +00000-0 +20963-3 0 00009
2 28414 97.6149 37.8226 0003728 301.5520 58.5343 15.05311032 00
| Epoch (UTC): | 18 January 2026 00:07:10 |
| Eccentricity: | 0.0003728 |
| inclination: | 97.6149° |
| perigee height: | 548 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 37.8226° |
| argument of perigee: | 301.5520° |
| revolutions per day: | 15.05311032 |
| mean anomaly at epoch: | 58.5343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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