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 36122U 09072B 22272.77585213 -.00000027 00000-0 40563-4 0 9997
2 36122 100.1963 240.3555 0008147 99.9901 260.2132 13.16372170614533
| Epoch (UTC): | 29 September 2022 18:37:13 |
| Eccentricity: | 0.0008147 |
| inclination: | 100.1963° |
| perigee height: | 1192 km |
| apogee height: | 1205 km |
| right ascension of ascending node: | 240.3555° |
| argument of perigee: | 99.9901° |
| revolutions per day: | 13.16372170 |
| mean anomaly at epoch: | 260.2132° |
| orbit number at epoch: | 61453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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