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 25140.87125292 .00000052 00000-0 44519-4 0 9994
2 00016 34.2827 359.6400 2023369 263.8454 72.9400 10.49575017647692
| Epoch (UTC): | 20 May 2025 20:54:36 |
| Eccentricity: | 0.2023369 |
| inclination: | 34.2827° |
| perigee height: | 650 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 359.6400° |
| argument of perigee: | 263.8454° |
| revolutions per day: | 10.49575017 |
| mean anomaly at epoch: | 72.9400° |
| orbit number at epoch: | 64769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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