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 24277U 96046A 19340.64216802 -.00000018 +00000-0 +10977-4 0 9991
2 24277 098.8479 307.7453 0000961 157.5837 202.5387 14.29442095214925
| Epoch (UTC): | 06 December 2019 15:24:43 |
| Eccentricity: | 0.0000961 |
| inclination: | 98.8479° |
| perigee height: | 793 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 307.7453° |
| argument of perigee: | 157.5837° |
| revolutions per day: | 14.29442095 |
| mean anomaly at epoch: | 202.5387° |
| orbit number at epoch: | 21492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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