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 26104.26851295 +.00000000 +00000-0 +30197-3 0 00004
2 28485 20.5539 315.7531 0002396 121.0402 239.0279 15.62709347 04
| Epoch (UTC): | 14 April 2026 06:26:39 |
| Eccentricity: | 0.0002396 |
| inclination: | 20.5539° |
| perigee height: | 378 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 315.7531° |
| argument of perigee: | 121.0402° |
| revolutions per day: | 15.62709347 |
| mean anomaly at epoch: | 239.0279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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