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 33490U 09001A 19056.53597444 0.00000000 00000-0 00000-0 0 04
2 33490 5.4128 32.0322 0004870 8.6807 351.3536 1.00270000 07
| Epoch (UTC): | 25 February 2019 12:51:48 |
| Eccentricity: | 0.0004870 |
| inclination: | 5.4128° |
| perigee height: | 35766 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 32.0322° |
| argument of perigee: | 8.6807° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 351.3536° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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