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 28352U 26159.61487397 +.00000000 +00000-0 +43134-4 0 00000
2 28352 70.9937 117.3876 0008790 170.1672 189.9623 14.12133765 09
| Epoch (UTC): | 08 June 2026 14:45:25 |
| Eccentricity: | 0.0008790 |
| inclination: | 70.9937° |
| perigee height: | 846 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 117.3876° |
| argument of perigee: | 170.1672° |
| revolutions per day: | 14.12133765 |
| mean anomaly at epoch: | 189.9623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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