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 26998U 01055B 18112.42715840 +.00000149 +00000-0 +20318-4 0 9991
2 26998 074.0728 059.7338 0001657 299.3629 060.7386 14.88009937887426
| Epoch (UTC): | 22 April 2018 10:15:06 |
| Eccentricity: | 0.0001657 |
| inclination: | 74.0728° |
| perigee height: | 603 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 59.7338° |
| argument of perigee: | 299.3629° |
| revolutions per day: | 14.88009937 |
| mean anomaly at epoch: | 60.7386° |
| orbit number at epoch: | 88742 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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