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 41384U 26153.00489699 +.00000000 +00000-0 +00000-0 0 00005
2 41384 5.3111 97.1235 0016757 187.0701 0.5168 1.00275291 07
| Epoch (UTC): | 02 June 2026 00:07:03 |
| Eccentricity: | 0.0016757 |
| inclination: | 5.3111° |
| perigee height: | 35715 km |
| apogee height: | 35856 km |
| right ascension of ascending node: | 97.1235° |
| argument of perigee: | 187.0701° |
| revolutions per day: | 1.00275291 |
| mean anomaly at epoch: | 0.5168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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