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 27868U 03037A 23088.47211784 .00000055 00000-0 31713-3 0 9997
2 27868 82.4768 347.0338 0022309 106.3768 253.9766 12.45153975891326
| Epoch (UTC): | 29 March 2023 11:19:50 |
| Eccentricity: | 0.0022309 |
| inclination: | 82.4768° |
| perigee height: | 1467 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 347.0338° |
| argument of perigee: | 106.3768° |
| revolutions per day: | 12.45153975 |
| mean anomaly at epoch: | 253.9766° |
| orbit number at epoch: | 89132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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