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 42017U 17008BX 22179.71320002 .00009237 00000-0 27461-3 0 9990
2 42017 97.2684 245.6651 0005163 184.1202 176.0000 15.34956071298806
| Epoch (UTC): | 28 June 2022 17:07:00 |
| Eccentricity: | 0.0005163 |
| inclination: | 97.2684° |
| perigee height: | 457 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 245.6651° |
| argument of perigee: | 184.1202° |
| revolutions per day: | 15.34956071 |
| mean anomaly at epoch: | 176.0000° |
| orbit number at epoch: | 29880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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