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 22148.82089622 .00023879 00000-0 28683-3 0 9999
2 48274 41.4723 336.6563 0001300 93.3425 31.7992 15.60312366 61742
| Epoch (UTC): | 28 May 2022 19:42:05 |
| Eccentricity: | 0.0001300 |
| inclination: | 41.4723° |
| perigee height: | 386 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 336.6563° |
| argument of perigee: | 93.3425° |
| revolutions per day: | 15.60312366 |
| mean anomaly at epoch: | 31.7992° |
| orbit number at epoch: | 6174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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