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 12998U 81120B 22223.26585709 -.00000039 00000-0 -57395-3 0 9990
2 12998 82.9617 162.1687 0019922 114.4282 44.7521 12.03165565785085
| Epoch (UTC): | 11 August 2022 06:22:50 |
| Eccentricity: | 0.0019922 |
| inclination: | 82.9617° |
| perigee height: | 1650 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 162.1687° |
| argument of perigee: | 114.4282° |
| revolutions per day: | 12.03165565 |
| mean anomaly at epoch: | 44.7521° |
| orbit number at epoch: | 78508 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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