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 39084U 26088.16240404 +.00000000 +00000-0 +98974-4 0 00003
2 39084 98.1884 159.5652 0001189 94.1313 266.0022 14.57128339 08
| Epoch (UTC): | 29 March 2026 03:53:51 |
| Eccentricity: | 0.0001189 |
| inclination: | 98.1884° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 159.5652° |
| argument of perigee: | 94.1313° |
| revolutions per day: | 14.57128339 |
| mean anomaly at epoch: | 266.0022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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