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 is defined by the following mean orbital elements,
1 33244U 08036A 24239.86760012 0.00028000 00000-0 85149-3 0 06
2 33244 98.1202 342.4152 0003147 93.0747 266.9252 15.34052506 09
| Epoch (UTC): | 26 August 2024 20:49:20 |
| Eccentricity: | 0.0003147 |
| inclination: | 98.1202° |
| perigee height: | 461 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 342.4152° |
| argument of perigee: | 93.0747° |
| revolutions per day: | 15.34052506 |
| mean anomaly at epoch: | 266.9252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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