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 00016U 26043.77828993 +.00000000 +00000-0 +49676-4 0 00004
2 00016 34.2748 304.8067 2021857 315.1500 30.2087 10.49577042 04
| Epoch (UTC): | 12 February 2026 18:40:44 |
| Eccentricity: | 0.2021857 |
| inclination: | 34.2748° |
| perigee height: | 652 km |
| apogee height: | 4215 km |
| right ascension of ascending node: | 304.8067° |
| argument of perigee: | 315.1500° |
| revolutions per day: | 10.49577042 |
| mean anomaly at epoch: | 30.2087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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