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 3900U 68097BM 23156.00373346 .00002309 00000-0 39268-3 0 9990
2 3900 62.2188 0.0360 0328687 283.1966 73.2627 14.42052262726829
Epoch (UTC): | 05 June 2023 00:05:22 |
Eccentricity: | 0.0328687 |
inclination: | 62.2188° |
perigee height: | 517 km |
apogee height: | 986 km |
right ascension of ascending node: | 0.0360° |
argument of perigee: | 283.1966° |
revolutions per day: | 14.42052262 |
mean anomaly at epoch: | 73.2627° |
orbit number at epoch: | 72682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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