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 42834U 17042K 22280.11948534 .00003573 00000-0 35251-3 0 9991
2 42834 97.4096 128.7210 0013180 1.4205 358.7050 14.92518062284789
| Epoch (UTC): | 07 October 2022 02:52:03 |
| Eccentricity: | 0.0013180 |
| inclination: | 97.4096° |
| perigee height: | 581 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 128.7210° |
| argument of perigee: | 1.4205° |
| revolutions per day: | 14.92518062 |
| mean anomaly at epoch: | 358.7050° |
| orbit number at epoch: | 28478 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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