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 22181.33848948 .00010583 00000-0 12802-3 0 9990
2 48274 41.4705 138.9361 0003073 349.2202 139.8044 15.60625152 66828
| Epoch (UTC): | 30 June 2022 08:07:25 |
| Eccentricity: | 0.0003073 |
| inclination: | 41.4705° |
| perigee height: | 384 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 138.9361° |
| argument of perigee: | 349.2202° |
| revolutions per day: | 15.60625152 |
| mean anomaly at epoch: | 139.8044° |
| orbit number at epoch: | 6682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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