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 26107.65905780 +.00000000 +00000-0 +00000-0 0 00009
2 41384 5.1963 98.1784 0017362 190.9576 186.3667 1.00269667 03
| Epoch (UTC): | 17 April 2026 15:49:02 |
| Eccentricity: | 0.0017362 |
| inclination: | 5.1963° |
| perigee height: | 35714 km |
| apogee height: | 35860 km |
| right ascension of ascending node: | 98.1784° |
| argument of perigee: | 190.9576° |
| revolutions per day: | 1.00269667 |
| mean anomaly at epoch: | 186.3667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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