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 23155.95077603 .00000258 00000-0 12537-3 0 9990
2 25338 98.6061 185.2165 0010114 356.7354 3.3759 14.26326769303268
| Epoch (UTC): | 04 June 2023 22:49:07 |
| Eccentricity: | 0.0010114 |
| inclination: | 98.6061° |
| perigee height: | 797 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 185.2165° |
| argument of perigee: | 356.7354° |
| revolutions per day: | 14.26326769 |
| mean anomaly at epoch: | 3.3759° |
| orbit number at epoch: | 30326 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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