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 37386U 11014A 25177.92133703 0.00000052 00000-0 67719-4 0 08
2 37386 63.4299 108.5520 0333557 357.5501 2.1892 13.40973991 03
| Epoch (UTC): | 26 June 2025 22:06:43 |
| Eccentricity: | 0.0333557 |
| inclination: | 63.4299° |
| perigee height: | 856 km |
| apogee height: | 1355 km |
| right ascension of ascending node: | 108.5520° |
| argument of perigee: | 357.5501° |
| revolutions per day: | 13.40973991 |
| mean anomaly at epoch: | 2.1892° |
| 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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