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 23271.18470471 .00020969 00000-0 22611-3 0 9994
2 48274 41.4726 249.1356 0008389 135.2649 224.8869 15.63128019137937
| Epoch (UTC): | 28 September 2023 04:25:58 |
| Eccentricity: | 0.0008389 |
| inclination: | 41.4726° |
| perigee height: | 373 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 249.1356° |
| argument of perigee: | 135.2649° |
| revolutions per day: | 15.63128019 |
| mean anomaly at epoch: | 224.8869° |
| orbit number at epoch: | 13793 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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