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 26018.64344058 +.00000000 +00000-0 +26436-4 0 00002
2 22676 74.0399 200.6708 0018381 183.0971 177.0071 14.35232158 07
| Epoch (UTC): | 18 January 2026 15:26:33 |
| Eccentricity: | 0.0018381 |
| inclination: | 74.0399° |
| perigee height: | 761 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 200.6708° |
| argument of perigee: | 183.0971° |
| revolutions per day: | 14.35232158 |
| mean anomaly at epoch: | 177.0071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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