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 12046U 26150.27102093 +.00000000 +00000-0 +00000-0 0 00004
2 12046 8.0256 304.6294 0003467 113.6853 246.3379 0.98953034 06
| Epoch (UTC): | 30 May 2026 06:30:16 |
| Eccentricity: | 0.0003467 |
| inclination: | 8.0256° |
| perigee height: | 36146 km |
| apogee height: | 36175 km |
| right ascension of ascending node: | 304.6294° |
| argument of perigee: | 113.6853° |
| revolutions per day: | 0.98953034 |
| mean anomaly at epoch: | 246.3379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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