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 is defined by the following mean orbital elements,
1 42700U 98067LH 19058.65367074 +.07524467 +12395-4 +57474-3 0 9993
2 42700 051.6026 103.5658 0000534 029.5264 063.1633 16.39608965102506
| Epoch (UTC): | 27 February 2019 15:41:17 |
| Eccentricity: | 0.0000534 |
| inclination: | 51.6026° |
| perigee height: | 166 km |
| apogee height: | 167 km |
| right ascension of ascending node: | 103.5658° |
| argument of perigee: | 29.5264° |
| revolutions per day: | 16.39608965 |
| mean anomaly at epoch: | 63.1633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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