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 12849U 26017.97903326 +.00000000 +00000-0 +10266-3 0 00000
2 12849 82.4874 271.6245 0869080 233.8910 117.8746 13.57859354 07
| Epoch (UTC): | 17 January 2026 23:29:48 |
| Eccentricity: | 0.0869080 |
| inclination: | 82.4874° |
| perigee height: | 398 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 271.6245° |
| argument of perigee: | 233.8910° |
| revolutions per day: | 13.57859354 |
| mean anomaly at epoch: | 117.8746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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