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 02701U 65048E 22181.33149081 .00000186 00000-0 22354-3 0 9990
2 02701 89.9136 303.6124 0063275 205.7481 207.9179 13.62738475824068
Epoch (UTC): | 30 June 2022 07:57:20 |
Eccentricity: | 0.0063275 |
inclination: | 89.9136° |
perigee height: | 979 km |
apogee height: | 1072 km |
right ascension of ascending node: | 303.6124° |
argument of perigee: | 205.7481° |
revolutions per day: | 13.62738475 |
mean anomaly at epoch: | 207.9179° |
orbit number at epoch: | 82406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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