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 25197.93333347 .00001006 00000-0 41729-3 0 9995
2 00020 33.3435 33.1602 1641120 57.4114 317.4440 11.60752302445628
| Epoch (UTC): | 16 July 2025 22:24:00 |
| Eccentricity: | 0.1641120 |
| inclination: | 33.3435° |
| perigee height: | 509 km |
| apogee height: | 3214 km |
| right ascension of ascending node: | 33.1602° |
| argument of perigee: | 57.4114° |
| revolutions per day: | 11.60752302 |
| mean anomaly at epoch: | 317.4440° |
| orbit number at epoch: | 44562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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