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 22178.79805045 .00000822 00000-0 67787-4 0 9991
2 29228 69.9355 102.6535 0002976 2.8057 357.3120 15.03264727883962
| Epoch (UTC): | 27 June 2022 19:09:11 |
| Eccentricity: | 0.0002976 |
| inclination: | 69.9355° |
| perigee height: | 555 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 102.6535° |
| argument of perigee: | 2.8057° |
| revolutions per day: | 15.03264727 |
| mean anomaly at epoch: | 357.3120° |
| orbit number at epoch: | 88396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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