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 12997U 81120A 22138.18898896 .00000040 00000-0 30429-3 0 9998
2 12997 82.9631 11.4881 0058513 147.4345 333.8554 12.15832146793500
| Epoch (UTC): | 18 May 2022 04:32:08 |
| Eccentricity: | 0.0058513 |
| inclination: | 82.9631° |
| perigee height: | 1564 km |
| apogee height: | 1657 km |
| right ascension of ascending node: | 11.4881° |
| argument of perigee: | 147.4345° |
| revolutions per day: | 12.15832146 |
| mean anomaly at epoch: | 333.8554° |
| orbit number at epoch: | 79350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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