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 15378U 84112A 24357.62235672 -.00000048 00000-0 36411-4 0 9996
2 15378 64.9931 23.3669 0043367 191.4746 168.5329 13.83669703 30050
| Epoch (UTC): | 22 December 2024 14:56:11 |
| Eccentricity: | 0.0043367 |
| inclination: | 64.9931° |
| perigee height: | 919 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 23.3669° |
| argument of perigee: | 191.4746° |
| revolutions per day: | 13.83669703 |
| mean anomaly at epoch: | 168.5329° |
| orbit number at epoch: | 3005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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