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 22488U 26129.53859852 +.00000000 +00000-0 +61084-5 0 00006
2 22488 82.9436 180.7125 0026693 119.2492 349.5848 13.78000130 00
| Epoch (UTC): | 09 May 2026 12:55:34 |
| Eccentricity: | 0.0026693 |
| inclination: | 82.9436° |
| perigee height: | 951 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 180.7125° |
| argument of perigee: | 119.2492° |
| revolutions per day: | 13.78000130 |
| mean anomaly at epoch: | 349.5848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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