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 26061U 00004A 19083.19157396 .00000048 00000-0 33281-4 0 9994
2 26061 100.2248 256.2346 0033666 189.1684 170.8888 14.41292435 6161
| Epoch (UTC): | 24 March 2019 04:35:51 |
| Eccentricity: | 0.0033666 |
| inclination: | 100.2248° |
| perigee height: | 730 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 256.2346° |
| argument of perigee: | 189.1684° |
| revolutions per day: | 14.41292435 |
| mean anomaly at epoch: | 170.8888° |
| orbit number at epoch: | 616 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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