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 22337.73902427 .00000102 00000-0 17677-3 0 9998
2 00299 67.1665 147.1389 0194119 177.0236 183.2040 13.68068515 52342
| Epoch (UTC): | 03 December 2022 17:44:11 |
| Eccentricity: | 0.0194119 |
| inclination: | 67.1665° |
| perigee height: | 863 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 147.1389° |
| argument of perigee: | 177.0236° |
| revolutions per day: | 13.68068515 |
| mean anomaly at epoch: | 183.2040° |
| orbit number at epoch: | 5234 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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