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 is defined by the following mean orbital elements,
1 36801U 10035G 19321.69550084 .99999999 34656-5 83064-3 0 9995
2 36801 98.0260 269.0390 0008874 110.9906 250.8370 16.53232176516325
| Epoch (UTC): | 17 November 2019 16:41:31 |
| Eccentricity: | 0.0008874 |
| inclination: | 98.0260° |
| perigee height: | 125 km |
| apogee height: | 136 km |
| right ascension of ascending node: | 269.0390° |
| argument of perigee: | 110.9906° |
| revolutions per day: | 16.53232176 |
| mean anomaly at epoch: | 250.8370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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