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 12508U 81053B 22139.59408570 .00000136 00000-0 12320-3 0 9999
2 12508 82.9592 251.6101 0036675 217.7200 142.1386 13.76395091 62484
| Epoch (UTC): | 19 May 2022 14:15:29 |
| Eccentricity: | 0.0036675 |
| inclination: | 82.9592° |
| perigee height: | 950 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 251.6101° |
| argument of perigee: | 217.7200° |
| revolutions per day: | 13.76395091 |
| mean anomaly at epoch: | 142.1386° |
| orbit number at epoch: | 6248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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