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 23078.58339620 .00000681 00000-0 32363-3 0 9993
2 27844 98.6810 87.1463 0010384 31.6111 328.5689 14.22684956 22997
| Epoch (UTC): | 19 March 2023 14:00:05 |
| Eccentricity: | 0.0010384 |
| inclination: | 98.6810° |
| perigee height: | 809 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 87.1463° |
| argument of perigee: | 31.6111° |
| revolutions per day: | 14.22684956 |
| mean anomaly at epoch: | 328.5689° |
| orbit number at epoch: | 2299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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