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 26109.06293368 +.00000000 +00000-0 +00000-0 0 00005
2 00836 52.6620 119.7842 5011327 278.2893 0.3694 0.23904628 06
| Epoch (UTC): | 19 April 2026 01:30:37 |
| Eccentricity: | 0.5011327 |
| inclination: | 52.6620° |
| perigee height: | 48332 km |
| apogee height: | 158248 km |
| right ascension of ascending node: | 119.7842° |
| argument of perigee: | 278.2893° |
| revolutions per day: | 0.23904628 |
| mean anomaly at epoch: | 0.3694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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