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 26048.72884064 +.00000000 +00000-0 +53944-4 0 00008
2 00016 34.2689 290.4918 2021380 336.0544 15.7573 10.49577334 06
| Epoch (UTC): | 17 February 2026 17:29:31 |
| Eccentricity: | 0.2021380 |
| inclination: | 34.2689° |
| perigee height: | 652 km |
| apogee height: | 4215 km |
| right ascension of ascending node: | 290.4918° |
| argument of perigee: | 336.0544° |
| revolutions per day: | 10.49577334 |
| mean anomaly at epoch: | 15.7573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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