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 22225.13271216 .00006462 00000-0 12042-3 0 9996
2 25544 51.6425 54.4836 0005702 116.2033 348.6352 15.50159232354012
| Epoch (UTC): | 13 August 2022 03:11:06 |
| Eccentricity: | 0.0005702 |
| inclination: | 51.6425° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 54.4836° |
| argument of perigee: | 116.2033° |
| revolutions per day: | 15.50159232 |
| mean anomaly at epoch: | 348.6352° |
| orbit number at epoch: | 35401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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