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 22803U 93059B 24276.58878393 .00000582 00000-0 31250-3 0 9992
2 22803 70.9920 34.1340 0019390 285.4838 74.4144 14.17078943605424
| Epoch (UTC): | 02 October 2024 14:07:50 |
| Eccentricity: | 0.0019390 |
| inclination: | 70.9920° |
| perigee height: | 821 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 34.1340° |
| argument of perigee: | 285.4838° |
| revolutions per day: | 14.17078943 |
| mean anomaly at epoch: | 74.4144° |
| orbit number at epoch: | 60542 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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