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 00836U 26113.24371772 +.00000000 +00000-0 +00000-0 0 00006
2 00836 52.6950 119.6649 5016637 278.1646 0.5744 0.23915773 01
| Epoch (UTC): | 23 April 2026 05:50:57 |
| Eccentricity: | 0.5016637 |
| inclination: | 52.6950° |
| perigee height: | 48257 km |
| apogee height: | 158255 km |
| right ascension of ascending node: | 119.6649° |
| argument of perigee: | 278.1646° |
| revolutions per day: | 0.23915773 |
| mean anomaly at epoch: | 0.5744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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