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 23270.03465384 .00027564 00000-0 29643-3 0 9994
2 48274 41.4726 256.1583 0008199 125.7178 234.4425 15.63074651137754
| Epoch (UTC): | 27 September 2023 00:49:54 |
| Eccentricity: | 0.0008199 |
| inclination: | 41.4726° |
| perigee height: | 373 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 256.1583° |
| argument of perigee: | 125.7178° |
| revolutions per day: | 15.63074651 |
| mean anomaly at epoch: | 234.4425° |
| orbit number at epoch: | 13775 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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