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 48274U 21035A 23337.54976731 .00017000 00000-0 18332-3 0 9994
2 48274 41.4700 204.5274 0007839 269.2201 90.7740 15.63242894148314
| Epoch (UTC): | 03 December 2023 13:11:39 |
| Eccentricity: | 0.0007839 |
| inclination: | 41.4700° |
| perigee height: | 373 km |
| apogee height: | 383 km |
| right ascension of ascending node: | 204.5274° |
| argument of perigee: | 269.2201° |
| revolutions per day: | 15.63242894 |
| mean anomaly at epoch: | 90.7740° |
| orbit number at epoch: | 14831 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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