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 00045U 26037.28432935 +.00000000 +00000-0 +14164-3 0 00005
2 00045 66.6950 346.4331 0255983 255.1923 102.0694 14.35862845 04
| Epoch (UTC): | 06 February 2026 06:49:26 |
| Eccentricity: | 0.0255983 |
| inclination: | 66.6950° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 346.4331° |
| argument of perigee: | 255.1923° |
| revolutions per day: | 14.35862845 |
| mean anomaly at epoch: | 102.0694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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