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 28381U 04028B 23152.41905490 .00000191 00000-0 17319-3 0 9996
2 28381 82.9560 158.0764 0032882 45.0881 63.6610 13.78371945948599
| Epoch (UTC): | 01 June 2023 10:03:26 |
| Eccentricity: | 0.0032882 |
| inclination: | 82.9560° |
| perigee height: | 945 km |
| apogee height: | 994 km |
| right ascension of ascending node: | 158.0764° |
| argument of perigee: | 45.0881° |
| revolutions per day: | 13.78371945 |
| mean anomaly at epoch: | 63.6610° |
| orbit number at epoch: | 94859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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