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 12904U 26162.59822215 +.00000000 +00000-0 +18741-3 0 00004
2 12904 81.1579 103.1981 0012186 336.4674 23.5999 15.22237841 05
| Epoch (UTC): | 11 June 2026 14:21:26 |
| Eccentricity: | 0.0012186 |
| inclination: | 81.1579° |
| perigee height: | 491 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 103.1981° |
| argument of perigee: | 336.4674° |
| revolutions per day: | 15.22237841 |
| mean anomaly at epoch: | 23.5999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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