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 27640U 03001A 22138.79611138 .00000138 00000-0 86792-4 0 9993
2 27640 98.7180 148.2555 0014190 178.2335 2.6364 14.19125872 2775
| Epoch (UTC): | 18 May 2022 19:06:24 |
| Eccentricity: | 0.0014190 |
| inclination: | 98.7180° |
| perigee height: | 818 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 148.2555° |
| argument of perigee: | 178.2335° |
| revolutions per day: | 14.19125872 |
| mean anomaly at epoch: | 2.6364° |
| orbit number at epoch: | 277 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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