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 28908U 26145.47641794 +.00000000 +00000-0 +16651-3 0 00002
2 28908 82.4677 322.1867 0007465 214.5029 159.7738 12.55600068 00
| Epoch (UTC): | 25 May 2026 11:26:02 |
| Eccentricity: | 0.0007465 |
| inclination: | 82.4677° |
| perigee height: | 1435 km |
| apogee height: | 1447 km |
| right ascension of ascending node: | 322.1867° |
| argument of perigee: | 214.5029° |
| revolutions per day: | 12.55600068 |
| mean anomaly at epoch: | 159.7738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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