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 12988U 81117B 22139.88656319 .00000545 00000-0 60960-4 0 9998
2 12988 82.5253 186.8674 0018738 32.0634 140.6453 14.84941343186560
| Epoch (UTC): | 19 May 2022 21:16:39 |
| Eccentricity: | 0.0018738 |
| inclination: | 82.5253° |
| perigee height: | 600 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 186.8674° |
| argument of perigee: | 32.0634° |
| revolutions per day: | 14.84941343 |
| mean anomaly at epoch: | 140.6453° |
| orbit number at epoch: | 18656 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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