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 23270.67357605 .00023291 00000-0 25089-3 0 9993
2 48274 41.4727 252.2564 0008284 131.1427 229.0129 15.63104802137858
| Epoch (UTC): | 27 September 2023 16:09:56 |
| Eccentricity: | 0.0008284 |
| inclination: | 41.4727° |
| perigee height: | 373 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 252.2564° |
| argument of perigee: | 131.1427° |
| revolutions per day: | 15.63104802 |
| mean anomaly at epoch: | 229.0129° |
| orbit number at epoch: | 13785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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