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 22178.83319145 .00011812 00000-0 14269-3 0 9998
2 48274 41.4699 154.1782 0003440 339.3135 96.1900 15.60572727 66432
| Epoch (UTC): | 27 June 2022 19:59:47 |
| Eccentricity: | 0.0003440 |
| inclination: | 41.4699° |
| perigee height: | 383 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 154.1782° |
| argument of perigee: | 339.3135° |
| revolutions per day: | 15.60572727 |
| mean anomaly at epoch: | 96.1900° |
| orbit number at epoch: | 6643 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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