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 04327U 26088.12836794 +.00000000 +00000-0 +50461-4 0 00003
2 04327 99.2784 30.1608 0005633 110.9021 260.3901 13.58731589 07
| Epoch (UTC): | 29 March 2026 03:04:50 |
| Eccentricity: | 0.0005633 |
| inclination: | 99.2784° |
| perigee height: | 1036 km |
| apogee height: | 1044 km |
| right ascension of ascending node: | 30.1608° |
| argument of perigee: | 110.9021° |
| revolutions per day: | 13.58731589 |
| mean anomaly at epoch: | 260.3901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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