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 29228U 06021A 19052.34080597 .00000051 00000-0 11154-4 0 9997
2 29228 69.9371 335.2048 0002564 160.9943 199.1314 15.02406983700333
| Epoch (UTC): | 21 February 2019 08:10:45 |
| Eccentricity: | 0.0002564 |
| inclination: | 69.9371° |
| perigee height: | 558 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 335.2048° |
| argument of perigee: | 160.9943° |
| revolutions per day: | 15.02406983 |
| mean anomaly at epoch: | 199.1314° |
| orbit number at epoch: | 70033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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