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 12443U 26068.48003028 +.00000000 +00000-0 +91955-4 0 00007
2 12443 74.0516 91.7874 0003178 138.5165 221.6230 14.36032703 08
| Epoch (UTC): | 09 March 2026 11:31:14 |
| Eccentricity: | 0.0003178 |
| inclination: | 74.0516° |
| perigee height: | 769 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 91.7874° |
| argument of perigee: | 138.5165° |
| revolutions per day: | 14.36032703 |
| mean anomaly at epoch: | 221.6230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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