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 23034.83568287 .00013008 00000-0 15386-3 0 9993
2 48274 41.4744 248.9770 0002330 139.3836 35.9497 15.61055020100978
| Epoch (UTC): | 03 February 2023 20:03:23 |
| Eccentricity: | 0.0002330 |
| inclination: | 41.4744° |
| perigee height: | 383 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 248.9770° |
| argument of perigee: | 139.3836° |
| revolutions per day: | 15.61055020 |
| mean anomaly at epoch: | 35.9497° |
| orbit number at epoch: | 10097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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