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 26144.30399159 +.00000000 +00000-0 +00000-0 0 00008
2 40889 54.9357 222.4171 0006406 263.0112 96.9692 1.67409242 00
| Epoch (UTC): | 24 May 2026 07:17:44 |
| Eccentricity: | 0.0006406 |
| inclination: | 54.9357° |
| perigee height: | 23563 km |
| apogee height: | 23602 km |
| right ascension of ascending node: | 222.4171° |
| argument of perigee: | 263.0112° |
| revolutions per day: | 1.67409242 |
| mean anomaly at epoch: | 96.9692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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