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 26072U 00007B 22221.58101548 .00038176 00000-0 17006-2 0 9996
2 26072 18.0920 2.4814 3854607 143.0726 250.9939 7.73396284477301
| Epoch (UTC): | 09 August 2022 13:56:39 |
| Eccentricity: | 0.3854607 |
| inclination: | 18.0920° |
| perigee height: | 259 km |
| apogee height: | 8586 km |
| right ascension of ascending node: | 2.4814° |
| argument of perigee: | 143.0726° |
| revolutions per day: | 7.73396284 |
| mean anomaly at epoch: | 250.9939° |
| orbit number at epoch: | 47730 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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