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 26133.03255461 +.00000000 +00000-0 +00000-0 0 00007
2 03307 120.8081 144.7193 0019148 284.6874 75.1607 6.42514541 04
| Epoch (UTC): | 13 May 2026 00:46:52 |
| Eccentricity: | 0.0019148 |
| inclination: | 120.8081° |
| perigee height: | 5821 km |
| apogee height: | 5867 km |
| right ascension of ascending node: | 144.7193° |
| argument of perigee: | 284.6874° |
| revolutions per day: | 6.42514541 |
| mean anomaly at epoch: | 75.1607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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