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 39153U 26045.97231315 +.00000000 +00000-0 +41661-3 0 00003
2 39153 98.1480 200.6591 0011891 186.7784 173.3277 14.96349623 04
| Epoch (UTC): | 14 February 2026 23:20:07 |
| Eccentricity: | 0.0011891 |
| inclination: | 98.1480° |
| perigee height: | 570 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 200.6591° |
| argument of perigee: | 186.7784° |
| revolutions per day: | 14.96349623 |
| mean anomaly at epoch: | 173.3277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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