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 22137.55863019 .00000060 00000-0 45804-4 0 9996
2 12508 82.9589 253.1180 0036574 223.6083 136.2182 13.76394353 62205
| Epoch (UTC): | 17 May 2022 13:24:25 |
| Eccentricity: | 0.0036574 |
| inclination: | 82.9589° |
| perigee height: | 950 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 253.1180° |
| argument of perigee: | 223.6083° |
| revolutions per day: | 13.76394353 |
| mean anomaly at epoch: | 136.2182° |
| orbit number at epoch: | 6220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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