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 38254U 12019A 23272.54635024 -.00000170 00000-0 00000+0 0 9998
2 38254 4.3641 62.1132 0003783 149.7266 258.7274 1.00272230 41730
| Epoch (UTC): | 29 September 2023 13:06:44 |
| Eccentricity: | 0.0003783 |
| inclination: | 4.3641° |
| perigee height: | 35770 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 62.1132° |
| argument of perigee: | 149.7266° |
| revolutions per day: | 1.00272230 |
| mean anomaly at epoch: | 258.7274° |
| orbit number at epoch: | 4173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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