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 29093U 06015B 22146.86342157 .00025358 00000-0 32739-3 0 9996
2 29093 97.6048 4.9674 0038560 262.1463 97.5414 15.58048174896191
| Epoch (UTC): | 26 May 2022 20:43:19 |
| Eccentricity: | 0.0038560 |
| inclination: | 97.6048° |
| perigee height: | 367 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 4.9674° |
| argument of perigee: | 262.1463° |
| revolutions per day: | 15.58048174 |
| mean anomaly at epoch: | 97.5414° |
| orbit number at epoch: | 89619 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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