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 23265.57531889 .00000595 00000-0 28434-3 0 9999
2 27844 98.6808 271.4210 0009356 197.0755 163.0109 14.22881579 49583
| Epoch (UTC): | 22 September 2023 13:48:27 |
| Eccentricity: | 0.0009356 |
| inclination: | 98.6808° |
| perigee height: | 809 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 271.4210° |
| argument of perigee: | 197.0755° |
| revolutions per day: | 14.22881579 |
| mean anomaly at epoch: | 163.0109° |
| orbit number at epoch: | 4958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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