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 23339.87667652 .00000255 00000-0 12377-3 0 9993
2 25338 98.5901 5.8755 0010590 166.9329 193.2128 14.26448640329487
| Epoch (UTC): | 05 December 2023 21:02:24 |
| Eccentricity: | 0.0010590 |
| inclination: | 98.5901° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 5.8755° |
| argument of perigee: | 166.9329° |
| revolutions per day: | 14.26448640 |
| mean anomaly at epoch: | 193.2128° |
| orbit number at epoch: | 32948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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