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 28118U 03057B 23090.91110172 .19201226 -86977-5 89195-3 0 9992
2 28118 28.0498 19.4849 0034963 217.8205 206.0984 16.38842028523649
| Epoch (UTC): | 31 March 2023 21:51:59 |
| Eccentricity: | 0.0034963 |
| inclination: | 28.0498° |
| perigee height: | 146 km |
| apogee height: | 192 km |
| right ascension of ascending node: | 19.4849° |
| argument of perigee: | 217.8205° |
| revolutions per day: | 16.38842028 |
| mean anomaly at epoch: | 206.0984° |
| orbit number at epoch: | 52364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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