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 26104.84301861 +.00000000 +00000-0 +30387-3 0 00008
2 28485 20.5537 311.3586 0002345 128.7392 231.3263 15.62742231 07
| Epoch (UTC): | 14 April 2026 20:13:56 |
| Eccentricity: | 0.0002345 |
| inclination: | 20.5537° |
| perigee height: | 378 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 311.3586° |
| argument of perigee: | 128.7392° |
| revolutions per day: | 15.62742231 |
| mean anomaly at epoch: | 231.3263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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