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 42169U 81053SH 24127.05190768 .00013584 00000-0 34811-2 0 9991
2 42169 82.8698 44.8868 0018976 172.9726 187.1742 14.50146059547223
| Epoch (UTC): | 06 May 2024 01:14:44 |
| Eccentricity: | 0.0018976 |
| inclination: | 82.8698° |
| perigee height: | 711 km |
| apogee height: | 738 km |
| right ascension of ascending node: | 44.8868° |
| argument of perigee: | 172.9726° |
| revolutions per day: | 14.50146059 |
| mean anomaly at epoch: | 187.1742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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