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 39161U 13021C 23080.45456666 .00003169 00000-0 49051-3 0 9993
2 39161 97.8801 155.2119 0008144 250.5454 109.4832 14.73893229530251
| Epoch (UTC): | 21 March 2023 10:54:34 |
| Eccentricity: | 0.0008144 |
| inclination: | 97.8801° |
| perigee height: | 643 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 155.2119° |
| argument of perigee: | 250.5454° |
| revolutions per day: | 14.73893229 |
| mean anomaly at epoch: | 109.4832° |
| orbit number at epoch: | 53025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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