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 27844U 03031E 23029.28099865 .00000391 00000-0 19426-3 0 9993
2 27844 98.6797 38.5733 0010143 162.3687 197.7845 14.22606064 16014
| Epoch (UTC): | 29 January 2023 06:44:38 |
| Eccentricity: | 0.0010143 |
| inclination: | 98.6797° |
| perigee height: | 809 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 38.5733° |
| argument of perigee: | 162.3687° |
| revolutions per day: | 14.22606064 |
| mean anomaly at epoch: | 197.7845° |
| orbit number at epoch: | 1601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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