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 39441U 26087.76773117 +.00000000 +00000-0 +40702-3 0 00002
2 39441 97.8832 27.6007 0065930 334.7799 25.0201 14.86287699 07
| Epoch (UTC): | 28 March 2026 18:25:31 |
| Eccentricity: | 0.0065930 |
| inclination: | 97.8832° |
| perigee height: | 563 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 27.6007° |
| argument of perigee: | 334.7799° |
| revolutions per day: | 14.86287699 |
| mean anomaly at epoch: | 25.0201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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