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 25134.97118244 .00000043 00000-0 31559-4 0 9997
2 00016 34.2802 16.6938 2023160 238.9457 99.6999 10.49574302647073
| Epoch (UTC): | 14 May 2025 23:18:30 |
| Eccentricity: | 0.2023160 |
| inclination: | 34.2802° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 16.6938° |
| argument of perigee: | 238.9457° |
| revolutions per day: | 10.49574302 |
| mean anomaly at epoch: | 99.6999° |
| orbit number at epoch: | 64707 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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