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 44865U 26144.43389308 +.00000000 +00000-0 +00000-0 0 00005
2 44865 56.5410 63.6095 0016630 310.6974 227.4211 1.86231454 08
| Epoch (UTC): | 24 May 2026 10:24:48 |
| Eccentricity: | 0.0016630 |
| inclination: | 56.5410° |
| perigee height: | 21482 km |
| apogee height: | 21574 km |
| right ascension of ascending node: | 63.6095° |
| argument of perigee: | 310.6974° |
| revolutions per day: | 1.86231454 |
| mean anomaly at epoch: | 227.4211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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