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 01778U 65096A 22181.59468547 .00000267 00000-0 78996-4 0 9999
2 01778 34.2568 25.1307 0749767 70.9460 297.0838 13.47161911769303
| Epoch (UTC): | 30 June 2022 14:16:20 |
| Eccentricity: | 0.0749767 |
| inclination: | 34.2568° |
| perigee height: | 523 km |
| apogee height: | 1642 km |
| right ascension of ascending node: | 25.1307° |
| argument of perigee: | 70.9460° |
| revolutions per day: | 13.47161911 |
| mean anomaly at epoch: | 297.0838° |
| orbit number at epoch: | 76930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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