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 26108.95785611 +.00000000 +00000-0 +10756-3 0 00009
2 27844 98.6763 118.2581 0009574 5.2865 354.8413 14.24297878 03
| Epoch (UTC): | 18 April 2026 22:59:18 |
| Eccentricity: | 0.0009574 |
| inclination: | 98.6763° |
| perigee height: | 804 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 118.2581° |
| argument of perigee: | 5.2865° |
| revolutions per day: | 14.24297878 |
| mean anomaly at epoch: | 354.8413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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