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 26056.06510816 +.00000000 +00000-0 +47543-3 0 00002
2 28485 20.5544 323.1884 0002554 214.0997 145.9283 15.58098952 00
| Epoch (UTC): | 25 February 2026 01:33:45 |
| Eccentricity: | 0.0002554 |
| inclination: | 20.5544° |
| perigee height: | 391 km |
| apogee height: | 395 km |
| right ascension of ascending node: | 323.1884° |
| argument of perigee: | 214.0997° |
| revolutions per day: | 15.58098952 |
| mean anomaly at epoch: | 145.9283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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