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 22676U 26074.47495122 +.00000000 +00000-0 +60972-4 0 00007
2 22676 74.0395 98.3409 0017078 61.7574 298.5300 14.35265026 00
| Epoch (UTC): | 15 March 2026 11:23:55 |
| Eccentricity: | 0.0017078 |
| inclination: | 74.0395° |
| perigee height: | 762 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 98.3409° |
| argument of perigee: | 61.7574° |
| revolutions per day: | 14.35265026 |
| mean anomaly at epoch: | 298.5300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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