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 23088.00747323 .00000766 00000-0 36126-3 0 9999
2 27844 98.6810 96.4333 0009851 5.3989 354.7294 14.22700517 24362
| Epoch (UTC): | 29 March 2023 00:10:45 |
| Eccentricity: | 0.0009851 |
| inclination: | 98.6810° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 96.4333° |
| argument of perigee: | 5.3989° |
| revolutions per day: | 14.22700517 |
| mean anomaly at epoch: | 354.7294° |
| orbit number at epoch: | 2436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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