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 23802U 96013A 19047.18594183 +.00000262 +00000-0 +00000-0 0 9994
2 23802 078.6765 257.2415 6831205 299.7003 009.9247 01.29844791110083
Epoch (UTC): | 16 February 2019 04:27:45 |
Eccentricity: | 0.6831205 |
inclination: | 78.6765° |
perigee height: | 4868 km |
apogee height: | 53357 km |
right ascension of ascending node: | 257.2415° |
argument of perigee: | 299.7003° |
revolutions per day: | 1.29844791 |
mean anomaly at epoch: | 9.9247° |
orbit number at epoch: | 11008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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