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 6153U 72065A 18267.59784743 +.00000034 +00000-0 +11742-4 0 9992
2 6153 035.0072 293.7115 0007362 257.6714 248.5008 14.57888214448429
| Epoch (UTC): | 24 September 2018 14:20:54 |
| Eccentricity: | 0.0007362 |
| inclination: | 35.0072° |
| perigee height: | 695 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 293.7115° |
| argument of perigee: | 257.6714° |
| revolutions per day: | 14.57888214 |
| mean anomaly at epoch: | 248.5008° |
| orbit number at epoch: | 44842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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