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 26069.69684125 +.00000000 +00000-0 +59556-3 0 00007
2 28485 20.5525 219.5373 0003943 43.5573 316.5183 15.59375243 05
| Epoch (UTC): | 10 March 2026 16:43:27 |
| Eccentricity: | 0.0003943 |
| inclination: | 20.5525° |
| perigee height: | 387 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 219.5373° |
| argument of perigee: | 43.5573° |
| revolutions per day: | 15.59375243 |
| mean anomaly at epoch: | 316.5183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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