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 22014.70787037 .00006419 00000-0 12245-3 0 9995
2 25544 51.6456 16.6326 0006618 22.6213 315.8466 15.49492476321370
| Epoch (UTC): | 14 January 2022 16:59:20 |
| Eccentricity: | 0.0006618 |
| inclination: | 51.6456° |
| perigee height: | 414 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 16.6326° |
| argument of perigee: | 22.6213° |
| revolutions per day: | 15.49492476 |
| mean anomaly at epoch: | 315.8466° |
| orbit number at epoch: | 32137 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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