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 37391U 11014B 25177.92125102 0.00000053 00000-0 68241-4 0 00
2 37391 63.4158 108.3882 0339289 357.9339 1.7098 13.40973228 09
| Epoch (UTC): | 26 June 2025 22:06:36 |
| Eccentricity: | 0.0339289 |
| inclination: | 63.4158° |
| perigee height: | 852 km |
| apogee height: | 1359 km |
| right ascension of ascending node: | 108.3882° |
| argument of perigee: | 357.9339° |
| revolutions per day: | 13.40973228 |
| mean anomaly at epoch: | 1.7098° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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