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 16012U 26039.50469659 +.00000000 +00000-0 +10284-3 0 00005
2 16012 74.0577 99.2653 0016157 291.3674 68.5756 14.37734779 07
| Epoch (UTC): | 08 February 2026 12:06:45 |
| Eccentricity: | 0.0016157 |
| inclination: | 74.0577° |
| perigee height: | 754 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 99.2653° |
| argument of perigee: | 291.3674° |
| revolutions per day: | 14.37734779 |
| mean anomaly at epoch: | 68.5756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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