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 is defined by the following mean orbital elements,
1 27842U 26110.26704910 +.00000000 +00000-0 +78422-4 0 00002
2 27842 98.6875 119.4183 0008698 337.7985 22.2816 14.23899061 02
| Epoch (UTC): | 20 April 2026 06:24:33 |
| Eccentricity: | 0.0008698 |
| inclination: | 98.6875° |
| perigee height: | 806 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 119.4183° |
| argument of perigee: | 337.7985° |
| revolutions per day: | 14.23899061 |
| mean anomaly at epoch: | 22.2816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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