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 25338U 98030A 23091.90281746 .00000377 00000-0 17521-3 0 9999
2 25338 98.6148 122.2355 0010661 170.4806 189.6578 14.26281634294139
| Epoch (UTC): | 01 April 2023 21:40:03 |
| Eccentricity: | 0.0010661 |
| inclination: | 98.6148° |
| perigee height: | 796 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 122.2355° |
| argument of perigee: | 170.4806° |
| revolutions per day: | 14.26281634 |
| mean anomaly at epoch: | 189.6578° |
| orbit number at epoch: | 29413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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