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 03307U 26088.05521287 +.00000000 +00000-0 +00000-0 0 00000
2 03307 120.8183 121.1229 0018810 284.6314 75.2203 6.42484411 05
| Epoch (UTC): | 29 March 2026 01:19:30 |
| Eccentricity: | 0.0018810 |
| inclination: | 120.8183° |
| perigee height: | 5821 km |
| apogee height: | 5867 km |
| right ascension of ascending node: | 121.1229° |
| argument of perigee: | 284.6314° |
| revolutions per day: | 6.42484411 |
| mean anomaly at epoch: | 75.2203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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