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 23335.17701388 .00000404 00000-0 18596-3 0 9992
2 25338 98.5903 1.2652 0010328 180.5264 179.5907 14.26445375329062
| Epoch (UTC): | 01 December 2023 04:14:53 |
| Eccentricity: | 0.0010328 |
| inclination: | 98.5903° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 1.2652° |
| argument of perigee: | 180.5264° |
| revolutions per day: | 14.26445375 |
| mean anomaly at epoch: | 179.5907° |
| orbit number at epoch: | 32906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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