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 22913U 26037.10364705 +.00000000 +00000-0 +25980-2 0 00000
2 22913 6.7356 309.8255 1675469 33.4787 336.0911 12.29273457 03
| Epoch (UTC): | 06 February 2026 02:29:15 |
| Eccentricity: | 0.1675469 |
| inclination: | 6.7356° |
| perigee height: | 224 km |
| apogee height: | 2881 km |
| right ascension of ascending node: | 309.8255° |
| argument of perigee: | 33.4787° |
| revolutions per day: | 12.29273457 |
| mean anomaly at epoch: | 336.0911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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