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 25197.17472915 -.00000079 00000-0 86240-5 0 9992
2 15378 64.9898 211.2145 0027296 109.3297 251.0718 13.83689544 58731
| Epoch (UTC): | 16 July 2025 04:11:36 |
| Eccentricity: | 0.0027296 |
| inclination: | 64.9898° |
| perigee height: | 931 km |
| apogee height: | 971 km |
| right ascension of ascending node: | 211.2145° |
| argument of perigee: | 109.3297° |
| revolutions per day: | 13.83689544 |
| mean anomaly at epoch: | 251.0718° |
| orbit number at epoch: | 5873 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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