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 23151.77860433 .00000193 00000-0 17491-3 0 9994
2 28381 82.9560 158.5525 0032910 46.8246 125.7177 13.78371740948507
| Epoch (UTC): | 31 May 2023 18:41:11 |
| Eccentricity: | 0.0032910 |
| inclination: | 82.9560° |
| perigee height: | 945 km |
| apogee height: | 994 km |
| right ascension of ascending node: | 158.5525° |
| argument of perigee: | 46.8246° |
| revolutions per day: | 13.78371740 |
| mean anomaly at epoch: | 125.7177° |
| orbit number at epoch: | 94850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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