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 22654U 26112.00871372 +.00000000 +00000-0 +00000-0 0 00002
2 22654 5.1945 48.6763 2854293 333.1212 251.5995 1.42203103 09
| Epoch (UTC): | 22 April 2026 00:12:32 |
| Eccentricity: | 0.2854293 |
| inclination: | 5.1945° |
| perigee height: | 17491 km |
| apogee height: | 36560 km |
| right ascension of ascending node: | 48.6763° |
| argument of perigee: | 333.1212° |
| revolutions per day: | 1.42203103 |
| mean anomaly at epoch: | 251.5995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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