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 22287U 92094B 22139.46955088 .00000435 00000-0 56542-4 0 9995
2 22287 82.5265 205.5754 0024002 205.8758 154.1256 14.78277412563025
| Epoch (UTC): | 19 May 2022 11:16:09 |
| Eccentricity: | 0.0024002 |
| inclination: | 82.5265° |
| perigee height: | 618 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 205.5754° |
| argument of perigee: | 205.8758° |
| revolutions per day: | 14.78277412 |
| mean anomaly at epoch: | 154.1256° |
| orbit number at epoch: | 56302 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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