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 26064.16083671 +.00000000 +00000-0 +84281-4 0 00004
2 12443 74.0518 99.7095 0003345 149.3858 210.7490 14.36030084 05
| Epoch (UTC): | 05 March 2026 03:51:36 |
| Eccentricity: | 0.0003345 |
| inclination: | 74.0518° |
| perigee height: | 769 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 99.7095° |
| argument of perigee: | 149.3858° |
| revolutions per day: | 14.36030084 |
| mean anomaly at epoch: | 210.7490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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