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 28096U 26018.48657742 +.00000000 +00000-0 +54426-4 0 00003
2 28096 63.6802 53.0622 0075442 123.2926 237.5356 13.41057770 03
| Epoch (UTC): | 18 January 2026 11:40:40 |
| Eccentricity: | 0.0075442 |
| inclination: | 63.6802° |
| perigee height: | 1049 km |
| apogee height: | 1162 km |
| right ascension of ascending node: | 53.0622° |
| argument of perigee: | 123.2926° |
| revolutions per day: | 13.41057770 |
| mean anomaly at epoch: | 237.5356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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