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 16909U 86061B 23027.11416343 -.00000093 00000-0 27004-4 0 9993
2 16909 50.0178 356.6022 0011076 254.3069 193.3173 12.44474076658056
| Epoch (UTC): | 27 January 2023 02:44:23 |
| Eccentricity: | 0.0011076 |
| inclination: | 50.0178° |
| perigee height: | 1479 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 356.6022° |
| argument of perigee: | 254.3069° |
| revolutions per day: | 12.44474076 |
| mean anomaly at epoch: | 193.3173° |
| orbit number at epoch: | 65805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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