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 25340.54759308 .00000109 00000-0 17207-3 0 9997
2 00016 34.2581 142.1181 2022686 27.0680 342.2296 10.49576227668673
| Epoch (UTC): | 06 December 2025 13:08:32 |
| Eccentricity: | 0.2022686 |
| inclination: | 34.2581° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 142.1181° |
| argument of perigee: | 27.0680° |
| revolutions per day: | 10.49576227 |
| mean anomaly at epoch: | 342.2296° |
| orbit number at epoch: | 66867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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