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 47311U 21002C 22175.81005836 .00005134 00000-0 21177-3 0 9993
2 47311 60.6860 334.5516 0017490 341.9566 18.0899 15.25406701 79581
| Epoch (UTC): | 24 June 2022 19:26:29 |
| Eccentricity: | 0.0017490 |
| inclination: | 60.6860° |
| perigee height: | 477 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 334.5516° |
| argument of perigee: | 341.9566° |
| revolutions per day: | 15.25406701 |
| mean anomaly at epoch: | 18.0899° |
| orbit number at epoch: | 7958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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