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 is defined by the following mean orbital elements,
1 43814U 18099BJ 21053.95883264 .25888781 26617-5 11832-1 0 9993
2 43814 97.7595 151.3588 0014519 299.9504 60.0343 16.21683976121934
| Epoch (UTC): | 22 February 2021 23:00:43 |
| Eccentricity: | 0.0014519 |
| inclination: | 97.7595° |
| perigee height: | 205 km |
| apogee height: | 224 km |
| right ascension of ascending node: | 151.3588° |
| argument of perigee: | 299.9504° |
| revolutions per day: | 16.21683976 |
| mean anomaly at epoch: | 60.0343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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