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 23150.55788370 .00021925 00000-0 27242-3 0 9999
2 48274 41.4740 262.9944 0003982 269.0498 90.9884 15.59456286119081
| Epoch (UTC): | 30 May 2023 13:23:21 |
| Eccentricity: | 0.0003982 |
| inclination: | 41.4740° |
| perigee height: | 386 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 262.9944° |
| argument of perigee: | 269.0498° |
| revolutions per day: | 15.59456286 |
| mean anomaly at epoch: | 90.9884° |
| orbit number at epoch: | 11908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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