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 20U 59007A 25163.16460124 .00000662 00000-0 25206-3 0 9996
2 20 33.3480 158.0710 1642890 231.4223 112.7593 11.60697611441616
| Epoch (UTC): | 12 June 2025 03:57:01 |
| Eccentricity: | 0.1642890 |
| inclination: | 33.3480° |
| perigee height: | 508 km |
| apogee height: | 3215 km |
| right ascension of ascending node: | 158.0710° |
| argument of perigee: | 231.4223° |
| revolutions per day: | 11.60697611 |
| mean anomaly at epoch: | 112.7593° |
| orbit number at epoch: | 44161 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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