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 27168U 02001A 23080.10327068 .00000087 00000-0 00000+0 0 9991
2 27168 9.7855 27.8496 0086265 351.8321 214.6828 1.00269257 19773
| Epoch (UTC): | 21 March 2023 02:28:42 |
| Eccentricity: | 0.0086265 |
| inclination: | 9.7855° |
| perigee height: | 35423 km |
| apogee height: | 36150 km |
| right ascension of ascending node: | 27.8496° |
| argument of perigee: | 351.8321° |
| revolutions per day: | 1.00269257 |
| mean anomaly at epoch: | 214.6828° |
| orbit number at epoch: | 1977 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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