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 42704U 98067LM 19059.52249959 +.04259319 +12249-4 +63401-3 0 9998
2 42704 051.6124 101.1040 0002748 040.6309 108.8739 16.33621154102537
| Epoch (UTC): | 28 February 2019 12:32:23 |
| Eccentricity: | 0.0002748 |
| inclination: | 51.6124° |
| perigee height: | 181 km |
| apogee height: | 184 km |
| right ascension of ascending node: | 101.1040° |
| argument of perigee: | 40.6309° |
| revolutions per day: | 16.33621154 |
| mean anomaly at epoch: | 108.8739° |
| orbit number at epoch: | 10253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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