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 00016U 58002A 25167.62178716 -.00000031 00000-0 -24738-4 0 9995
2 00016 34.2643 282.2877 2022998 16.7942 349.0740 10.49574931650504
| Epoch (UTC): | 16 June 2025 14:55:22 |
| Eccentricity: | 0.2022998 |
| inclination: | 34.2643° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 282.2877° |
| argument of perigee: | 16.7942° |
| revolutions per day: | 10.49574931 |
| mean anomaly at epoch: | 349.0740° |
| orbit number at epoch: | 65050 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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