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 27006U 01056F 25199.08262465 -.00000021 00000-0 27925-4 0 9999
2 27006 99.7411 356.4465 0013925 227.6428 240.9978 13.71077134181128
| Epoch (UTC): | 18 July 2025 01:58:58 |
| Eccentricity: | 0.0013925 |
| inclination: | 99.7411° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 356.4465° |
| argument of perigee: | 227.6428° |
| revolutions per day: | 13.71077134 |
| mean anomaly at epoch: | 240.9978° |
| orbit number at epoch: | 18112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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