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 27518U 02042D 22137.70345426 .00000034 00000-0 44338-3 0 9999
2 27518 28.8271 36.3757 7131795 123.1460 325.0229 2.36566935169974
| Epoch (UTC): | 17 May 2022 16:52:58 |
| Eccentricity: | 0.7131795 |
| inclination: | 28.8271° |
| perigee height: | 446 km |
| apogee height: | 34381 km |
| right ascension of ascending node: | 36.3757° |
| argument of perigee: | 123.1460° |
| revolutions per day: | 2.36566935 |
| mean anomaly at epoch: | 325.0229° |
| orbit number at epoch: | 16997 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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