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 23028.17388606 .00016283 00000-0 19279-3 0 9991
2 48274 41.4742 289.5256 0002385 60.2418 70.3822 15.60883300 99931
| Epoch (UTC): | 28 January 2023 04:10:23 |
| Eccentricity: | 0.0002385 |
| inclination: | 41.4742° |
| perigee height: | 383 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 289.5256° |
| argument of perigee: | 60.2418° |
| revolutions per day: | 15.60883300 |
| mean anomaly at epoch: | 70.3822° |
| orbit number at epoch: | 9993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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