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 23270.74001321 -.00000025 00000-0 56564-4 0 9990
2 15378 64.9906 113.2128 0055445 305.5286 54.0610 13.83613425967778
| Epoch (UTC): | 27 September 2023 17:45:37 |
| Eccentricity: | 0.0055445 |
| inclination: | 64.9906° |
| perigee height: | 910 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 113.2128° |
| argument of perigee: | 305.5286° |
| revolutions per day: | 13.83613425 |
| mean anomaly at epoch: | 54.0610° |
| orbit number at epoch: | 96777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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