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 36105U 09066B 22091.15461159 0.00006500 00000-0 32257-3 0 08
2 36105 97.3261 77.7070 0032626 15.3746 344.6253 15.17269400 00
| Epoch (UTC): | 01 April 2022 03:42:38 |
| Eccentricity: | 0.0032626 |
| inclination: | 97.3261° |
| perigee height: | 491 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 77.7070° |
| argument of perigee: | 15.3746° |
| revolutions per day: | 15.17269400 |
| mean anomaly at epoch: | 344.6253° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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