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 22277.16482100 .00013548 00000-0 24746-3 0 9999
2 25544 51.6425 156.6670 0003069 256.3783 244.5677 15.49707041362080
| Epoch (UTC): | 04 October 2022 03:57:20 |
| Eccentricity: | 0.0003069 |
| inclination: | 51.6425° |
| perigee height: | 415 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 156.6670° |
| argument of perigee: | 256.3783° |
| revolutions per day: | 15.49707041 |
| mean anomaly at epoch: | 244.5677° |
| orbit number at epoch: | 36208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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