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 23151.18972207 -.00000069 00000-0 17315-4 0 9995
2 15378 64.9933 62.6882 0046934 337.1446 22.7524 13.83605582950980
| Epoch (UTC): | 31 May 2023 04:33:11 |
| Eccentricity: | 0.0046934 |
| inclination: | 64.9933° |
| perigee height: | 917 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 62.6882° |
| argument of perigee: | 337.1446° |
| revolutions per day: | 13.83605582 |
| mean anomaly at epoch: | 22.7524° |
| orbit number at epoch: | 95098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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