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 00107U 61013A 22176.13243586 .00000910 00000-0 10344-3 0 9994
2 00107 28.7895 332.9673 0542216 10.4311 350.7023 14.10111798 70383
| Epoch (UTC): | 25 June 2022 03:10:42 |
| Eccentricity: | 0.0542216 |
| inclination: | 28.7895° |
| perigee height: | 466 km |
| apogee height: | 1251 km |
| right ascension of ascending node: | 332.9673° |
| argument of perigee: | 10.4311° |
| revolutions per day: | 14.10111798 |
| mean anomaly at epoch: | 350.7023° |
| orbit number at epoch: | 7038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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