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 27844U 03031E 22135.92885829 .00000317 00000-0 16184-3 0 9990
2 27844 98.6795 144.1059 0009608 189.0651 171.0355 14.22434507979243
| Epoch (UTC): | 15 May 2022 22:17:33 |
| Eccentricity: | 0.0009608 |
| inclination: | 98.6795° |
| perigee height: | 810 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 144.1059° |
| argument of perigee: | 189.0651° |
| revolutions per day: | 14.22434507 |
| mean anomaly at epoch: | 171.0355° |
| orbit number at epoch: | 97924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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