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 09904U 26047.23874951 +.00000000 +00000-0 +42267-4 0 00008
2 09904 81.2630 309.9752 0056470 48.4609 312.1383 14.07298185 08
| Epoch (UTC): | 16 February 2026 05:43:47 |
| Eccentricity: | 0.0056470 |
| inclination: | 81.2630° |
| perigee height: | 828 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 309.9752° |
| argument of perigee: | 48.4609° |
| revolutions per day: | 14.07298185 |
| mean anomaly at epoch: | 312.1383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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