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 22145.12929155 .00029195 00000-0 37789-3 0 9996
2 29093 97.6050 3.1161 0038603 269.0287 90.6545 15.57951512896023
| Epoch (UTC): | 25 May 2022 03:06:10 |
| Eccentricity: | 0.0038603 |
| inclination: | 97.6050° |
| perigee height: | 367 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 3.1161° |
| argument of perigee: | 269.0287° |
| revolutions per day: | 15.57951512 |
| mean anomaly at epoch: | 90.6545° |
| orbit number at epoch: | 89602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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