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 26159.19434933 +.00000000 +00000-0 +00000-0 0 00009
2 00836 52.8772 118.7365 5119465 276.4069 0.5219 0.23906814 06
| Epoch (UTC): | 08 June 2026 04:39:51 |
| Eccentricity: | 0.5119465 |
| inclination: | 52.8772° |
| perigee height: | 47143 km |
| apogee height: | 159424 km |
| right ascension of ascending node: | 118.7365° |
| argument of perigee: | 276.4069° |
| revolutions per day: | 0.23906814 |
| mean anomaly at epoch: | 0.5219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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