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 26073.49912990 +.00000000 +00000-0 +66856-4 0 00002
2 22676 74.0395 100.1298 0017048 63.9148 296.3756 14.35264772 04
| Epoch (UTC): | 14 March 2026 11:58:44 |
| Eccentricity: | 0.0017048 |
| inclination: | 74.0395° |
| perigee height: | 762 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 100.1298° |
| argument of perigee: | 63.9148° |
| revolutions per day: | 14.35264772 |
| mean anomaly at epoch: | 296.3756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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