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 26621U 00075C 18266.04661700 -.00000526 +00000-0 -46394-3 0 9990
2 26621 095.3995 100.1981 0712251 325.5919 030.0959 13.04181330848720
| Epoch (UTC): | 23 September 2018 01:07:07 |
| Eccentricity: | 0.0712251 |
| inclination: | 95.3995° |
| perigee height: | 703 km |
| apogee height: | 1789 km |
| right ascension of ascending node: | 100.1981° |
| argument of perigee: | 325.5919° |
| revolutions per day: | 13.04181330 |
| mean anomaly at epoch: | 30.0959° |
| orbit number at epoch: | 84872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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