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 12988U 81117B 24357.56182165 .00000919 00000-0 10080-3 0 9992
2 12988 82.5236 16.6851 0018774 129.1284 231.1606 14.86543689306212
| Epoch (UTC): | 22 December 2024 13:29:01 |
| Eccentricity: | 0.0018774 |
| inclination: | 82.5236° |
| perigee height: | 595 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 16.6851° |
| argument of perigee: | 129.1284° |
| revolutions per day: | 14.86543689 |
| mean anomaly at epoch: | 231.1606° |
| orbit number at epoch: | 30621 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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