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 28485U 26071.67983808 +.00000000 +00000-0 +52958-3 0 00007
2 28485 20.5517 204.4373 0003847 69.9332 290.1526 15.59560858 03
| Epoch (UTC): | 12 March 2026 16:18:58 |
| Eccentricity: | 0.0003847 |
| inclination: | 20.5517° |
| perigee height: | 386 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 204.4373° |
| argument of perigee: | 69.9332° |
| revolutions per day: | 15.59560858 |
| mean anomaly at epoch: | 290.1526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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