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 25189.89013552 -.00000036 00000-0 11687-4 0 9992
2 27006 99.7398 347.1319 0013739 252.4316 226.8283 13.71076931179866
Epoch (UTC): | 08 July 2025 21:21:47 |
Eccentricity: | 0.0013739 |
inclination: | 99.7398° |
perigee height: | 985 km |
apogee height: | 1006 km |
right ascension of ascending node: | 347.1319° |
argument of perigee: | 252.4316° |
revolutions per day: | 13.71076931 |
mean anomaly at epoch: | 226.8283° |
orbit number at epoch: | 17986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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