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 22825U 93061C 23028.71539841 .00000122 00000-0 64844-4 0 9996
2 22825 98.8621 69.2205 0009438 112.8577 247.3602 14.30236949530355
| Epoch (UTC): | 28 January 2023 17:10:10 |
| Eccentricity: | 0.0009438 |
| inclination: | 98.8621° |
| perigee height: | 784 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 69.2205° |
| argument of perigee: | 112.8577° |
| revolutions per day: | 14.30236949 |
| mean anomaly at epoch: | 247.3602° |
| orbit number at epoch: | 53035 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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