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 40889U 26105.47814955 +.00000000 +00000-0 +00000-0 0 00009
2 40889 54.9657 223.4453 0004687 268.4414 91.4761 1.67410740 02
| Epoch (UTC): | 15 April 2026 11:28:32 |
| Eccentricity: | 0.0004687 |
| inclination: | 54.9657° |
| perigee height: | 23568 km |
| apogee height: | 23596 km |
| right ascension of ascending node: | 223.4453° |
| argument of perigee: | 268.4414° |
| revolutions per day: | 1.67410740 |
| mean anomaly at epoch: | 91.4761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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