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 26110.29260097 +.00000000 +00000-0 +10144-3 0 00006
2 27844 98.6762 119.5763 0009488 1.4392 358.6813 14.24298412 06
| Epoch (UTC): | 20 April 2026 07:01:20 |
| Eccentricity: | 0.0009488 |
| inclination: | 98.6762° |
| perigee height: | 804 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 119.5763° |
| argument of perigee: | 1.4392° |
| revolutions per day: | 14.24298412 |
| mean anomaly at epoch: | 358.6813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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