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 29499U 06044A 22225.90026622 .00000802 00000-0 11472-3 0 9995
2 29499 98.4474 272.3280 0197614 187.5677 167.7271 14.67314097819094
| Epoch (UTC): | 13 August 2022 21:36:23 |
| Eccentricity: | 0.0197614 |
| inclination: | 98.4474° |
| perigee height: | 530 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 272.3280° |
| argument of perigee: | 187.5677° |
| revolutions per day: | 14.67314097 |
| mean anomaly at epoch: | 167.7271° |
| orbit number at epoch: | 81909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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