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 22221.81469878 .00000178 00000-0 99473-4 0 9994
2 27844 98.6793 228.6959 0008933 312.9886 47.0543 14.22477230991453
| Epoch (UTC): | 09 August 2022 19:33:09 |
| Eccentricity: | 0.0008933 |
| inclination: | 98.6793° |
| perigee height: | 810 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 228.6959° |
| argument of perigee: | 312.9886° |
| revolutions per day: | 14.22477230 |
| mean anomaly at epoch: | 47.0543° |
| orbit number at epoch: | 99145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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