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 00299U 61015CQ 22181.36065509 -.00000010 00000-0 62037-4 0 9995
2 00299 67.1669 149.2673 0200365 290.7667 67.2038 13.68027241 30959
| Epoch (UTC): | 30 June 2022 08:39:20 |
| Eccentricity: | 0.0200365 |
| inclination: | 67.1669° |
| perigee height: | 858 km |
| apogee height: | 1154 km |
| right ascension of ascending node: | 149.2673° |
| argument of perigee: | 290.7667° |
| revolutions per day: | 13.68027241 |
| mean anomaly at epoch: | 67.2038° |
| orbit number at epoch: | 3095 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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