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 42418U 00055TN 22278.13661767 .00003553 00000-0 18126-2 0 9993
2 42418 98.7532 348.9425 0014431 123.9293 236.3256 14.16255333339423
| Epoch (UTC): | 05 October 2022 03:16:43 |
| Eccentricity: | 0.0014431 |
| inclination: | 98.7532° |
| perigee height: | 827 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 348.9425° |
| argument of perigee: | 123.9293° |
| revolutions per day: | 14.16255333 |
| mean anomaly at epoch: | 236.3256° |
| orbit number at epoch: | 33942 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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