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 27944U 26145.55911623 +.00000000 +00000-0 +17405-4 0 00000
2 27944 98.4133 307.2928 0013486 105.5256 254.7436 14.63864340 03
| Epoch (UTC): | 25 May 2026 13:25:07 |
| Eccentricity: | 0.0013486 |
| inclination: | 98.4133° |
| perigee height: | 671 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 307.2928° |
| argument of perigee: | 105.5256° |
| revolutions per day: | 14.63864340 |
| mean anomaly at epoch: | 254.7436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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