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 00729U 26088.17188863 +.00000000 +00000-0 +62054-4 0 00008
2 00729 69.8984 104.4681 0014422 191.7007 168.3765 13.95217454 03
| Epoch (UTC): | 29 March 2026 04:07:31 |
| Eccentricity: | 0.0014422 |
| inclination: | 69.8984° |
| perigee height: | 900 km |
| apogee height: | 921 km |
| right ascension of ascending node: | 104.4681° |
| argument of perigee: | 191.7007° |
| revolutions per day: | 13.95217454 |
| mean anomaly at epoch: | 168.3765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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