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 21949U 92023A 18281.06506085 0.00000000 00000-0 00000-0 0 04
2 21949 85.0077 253.1715 0002500 165.9863 194.0135 14.31415867 06
| Epoch (UTC): | 08 October 2018 01:33:41 |
| Eccentricity: | 0.0002500 |
| inclination: | 85.0077° |
| perigee height: | 785 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 253.1715° |
| argument of perigee: | 165.9863° |
| revolutions per day: | 14.31415867 |
| mean anomaly at epoch: | 194.0135° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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