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 38857U 12055A 23332.39055501 .00000034 00000-0 00000+0 0 9991
2 38857 55.3203 127.1537 0002389 237.3788 122.5663 1.70473601 69264
| Epoch (UTC): | 28 November 2023 09:22:23 |
| Eccentricity: | 0.0002389 |
| inclination: | 55.3203° |
| perigee height: | 23215 km |
| apogee height: | 23229 km |
| right ascension of ascending node: | 127.1537° |
| argument of perigee: | 237.3788° |
| revolutions per day: | 1.70473601 |
| mean anomaly at epoch: | 122.5663° |
| orbit number at epoch: | 6926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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