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 23439U 94085A 22178.95101319 -.00000039 00000-0 10000-3 0 9993
2 23439 64.8154 128.6361 0168154 270.7358 87.4300 11.27572694132670
| Epoch (UTC): | 27 June 2022 22:49:27 |
| Eccentricity: | 0.0168154 |
| inclination: | 64.8154° |
| perigee height: | 1881 km |
| apogee height: | 2163 km |
| right ascension of ascending node: | 128.6361° |
| argument of perigee: | 270.7358° |
| revolutions per day: | 11.27572694 |
| mean anomaly at epoch: | 87.4300° |
| orbit number at epoch: | 13267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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