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 27844U 26154.54951728 +.00000000 +00000-0 +16425-3 0 00008
2 27844 98.6736 163.2800 0008691 219.4250 140.6297 14.24327019 05
| Epoch (UTC): | 03 June 2026 13:11:18 |
| Eccentricity: | 0.0008691 |
| inclination: | 98.6736° |
| perigee height: | 805 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 163.2800° |
| argument of perigee: | 219.4250° |
| revolutions per day: | 14.24327019 |
| mean anomaly at epoch: | 140.6297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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