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 00020U 59007A 25173.23139617 .00000528 00000-0 19975-3 0 9992
2 00020 33.3519 121.9110 1642999 285.2481 57.2862 11.60710999442758
| Epoch (UTC): | 22 June 2025 05:33:12 |
| Eccentricity: | 0.1642999 |
| inclination: | 33.3519° |
| perigee height: | 508 km |
| apogee height: | 3215 km |
| right ascension of ascending node: | 121.9110° |
| argument of perigee: | 285.2481° |
| revolutions per day: | 11.60710999 |
| mean anomaly at epoch: | 57.2862° |
| orbit number at epoch: | 44275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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