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 data is extracted from the following two-line orbital elements,
1 25520U 98064B 22222.35687964 .00003115 00000-0 91356-4 0 9997
2 25520 28.4404 116.6909 0004710 14.0036 346.0690 15.31723765322438
| Epoch (UTC): | 10 August 2022 08:33:54 |
| Eccentricity: | 0.0004710 |
| inclination: | 28.4404° |
| perigee height: | 467 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 116.6909° |
| argument of perigee: | 14.0036° |
| revolutions per day: | 15.31723765 |
| mean anomaly at epoch: | 346.0690° |
| orbit number at epoch: | 32243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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