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 24261.15116353 .00011830 00000-0 16715-2 0 9992
2 39161 97.8207 324.8207 0007541 294.5222 65.5202 14.77280473610701
| Epoch (UTC): | 17 September 2024 03:37:40 |
| Eccentricity: | 0.0007541 |
| inclination: | 97.8207° |
| perigee height: | 632 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 324.8207° |
| argument of perigee: | 294.5222° |
| revolutions per day: | 14.77280473 |
| mean anomaly at epoch: | 65.5202° |
| orbit number at epoch: | 61070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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