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 22140.81145174 .00025708 00000-0 31329-3 0 9999
2 48274 41.4713 25.3473 0003052 11.4809 70.8236 15.59899051 60491
| Epoch (UTC): | 20 May 2022 19:28:29 |
| Eccentricity: | 0.0003052 |
| inclination: | 41.4713° |
| perigee height: | 386 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 25.3473° |
| argument of perigee: | 11.4809° |
| revolutions per day: | 15.59899051 |
| mean anomaly at epoch: | 70.8236° |
| orbit number at epoch: | 6049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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