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 26019.12946448 +.00000000 +00000-0 -10167-3 0 00005
2 00016 34.2742 16.0565 2022591 211.1301 135.2223 10.49574115 09
| Epoch (UTC): | 19 January 2026 03:06:25 |
| Eccentricity: | 0.2022591 |
| inclination: | 34.2742° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 16.0565° |
| argument of perigee: | 211.1301° |
| revolutions per day: | 10.49574115 |
| mean anomaly at epoch: | 135.2223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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