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 04362U 70025A 23079.73629490 -.00000001 00000-0 74318-4 0 9999
2 04362 99.9545 357.1311 0007696 10.0998 44.7530 13.44651498597654
| Epoch (UTC): | 20 March 2023 17:40:15 |
| Eccentricity: | 0.0007696 |
| inclination: | 99.9545° |
| perigee height: | 1086 km |
| apogee height: | 1098 km |
| right ascension of ascending node: | 357.1311° |
| argument of perigee: | 10.0998° |
| revolutions per day: | 13.44651498 |
| mean anomaly at epoch: | 44.7530° |
| orbit number at epoch: | 59765 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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