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 26040.26065426 +.00000000 +00000-0 +84213-4 0 00003
2 28096 63.6819 358.0917 0074420 120.8101 240.0277 13.41059901 08
| Epoch (UTC): | 09 February 2026 06:15:20 |
| Eccentricity: | 0.0074420 |
| inclination: | 63.6819° |
| perigee height: | 1050 km |
| apogee height: | 1161 km |
| right ascension of ascending node: | 358.0917° |
| argument of perigee: | 120.8101° |
| revolutions per day: | 13.41059901 |
| mean anomaly at epoch: | 240.0277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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