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 29528U 06051C 19348.74932661 +.00000057 +00000-0 -21029-3 0 9991
2 29528 051.1139 159.2464 6053663 095.7804 252.8545 03.64257717174297
Epoch (UTC): | 14 December 2019 17:59:01 |
Eccentricity: | 0.6053663 |
inclination: | 51.1139° |
perigee height: | 663 km |
apogee height: | 22266 km |
right ascension of ascending node: | 159.2464° |
argument of perigee: | 95.7804° |
revolutions per day: | 3.64257717 |
mean anomaly at epoch: | 252.8545° |
orbit number at epoch: | 17429 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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