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 25544U 98067A 22024.15026959 .00005618 00000-0 10778-3 0 9993
2 25544 51.6440 329.8886 0006748 56.4665 70.0126 15.49607565322846
| Epoch (UTC): | 24 January 2022 03:36:23 |
| Eccentricity: | 0.0006748 |
| inclination: | 51.6440° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 329.8886° |
| argument of perigee: | 56.4665° |
| revolutions per day: | 15.49607565 |
| mean anomaly at epoch: | 70.0126° |
| orbit number at epoch: | 32284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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