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 22671U 26068.43533903 +.00000000 +00000-0 +73201-3 0 00009
2 22671 62.9093 156.1979 4936481 31.5295 350.4241 5.65113385 03
| Epoch (UTC): | 09 March 2026 10:26:53 |
| Eccentricity: | 0.4936481 |
| inclination: | 62.9093° |
| perigee height: | 363 km |
| apogee height: | 13508 km |
| right ascension of ascending node: | 156.1979° |
| argument of perigee: | 31.5295° |
| revolutions per day: | 5.65113385 |
| mean anomaly at epoch: | 350.4241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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