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 25082.53930258 .00000271 00000-0 39313-3 0 9996
2 00016 34.2599 168.3463 2021716 17.4723 348.6234 10.49558215641567
| Epoch (UTC): | 23 March 2025 12:56:35 |
| Eccentricity: | 0.2021716 |
| inclination: | 34.2599° |
| perigee height: | 652 km |
| apogee height: | 4215 km |
| right ascension of ascending node: | 168.3463° |
| argument of perigee: | 17.4723° |
| revolutions per day: | 10.49558215 |
| mean anomaly at epoch: | 348.6234° |
| orbit number at epoch: | 64156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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