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 23088.51097336 -.00000010 00000-0 86981-4 0 9995
2 36122 100.2293 54.9309 0008046 49.2967 310.8844 13.16380361638319
| Epoch (UTC): | 29 March 2023 12:15:48 |
| Eccentricity: | 0.0008046 |
| inclination: | 100.2293° |
| perigee height: | 1192 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 54.9309° |
| argument of perigee: | 49.2967° |
| revolutions per day: | 13.16380361 |
| mean anomaly at epoch: | 310.8844° |
| orbit number at epoch: | 63831 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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