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 02825U 67053B 22144.86768848 .00000070 00000-0 88073-4 0 9993
2 02825 69.9734 18.7650 0009358 293.6152 66.3971 13.97219557884749
| Epoch (UTC): | 24 May 2022 20:49:28 |
| Eccentricity: | 0.0009358 |
| inclination: | 69.9734° |
| perigee height: | 896 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 18.7650° |
| argument of perigee: | 293.6152° |
| revolutions per day: | 13.97219557 |
| mean anomaly at epoch: | 66.3971° |
| orbit number at epoch: | 88474 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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