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 44864U 26142.41824409 +.00000000 +00000-0 +00000-0 0 00006
2 44864 56.5381 63.6419 0018941 297.3914 239.7429 1.86231321 06
| Epoch (UTC): | 22 May 2026 10:02:16 |
| Eccentricity: | 0.0018941 |
| inclination: | 56.5381° |
| perigee height: | 21475 km |
| apogee height: | 21581 km |
| right ascension of ascending node: | 63.6419° |
| argument of perigee: | 297.3914° |
| revolutions per day: | 1.86231321 |
| mean anomaly at epoch: | 239.7429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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