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 26046.72954808 +.00000000 +00000-0 +79321-4 0 00007
2 00016 34.2714 296.2736 2021564 327.6113 21.4727 10.49577278 01
| Epoch (UTC): | 15 February 2026 17:30:32 |
| Eccentricity: | 0.2021564 |
| inclination: | 34.2714° |
| perigee height: | 652 km |
| apogee height: | 4215 km |
| right ascension of ascending node: | 296.2736° |
| argument of perigee: | 327.6113° |
| revolutions per day: | 10.49577278 |
| mean anomaly at epoch: | 21.4727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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