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 44859U 26145.36281058 +.00000000 +00000-0 +12362-3 0 00001
2 44859 36.9657 175.9843 0004054 44.1485 315.9584 15.11677889 02
| Epoch (UTC): | 25 May 2026 08:42:26 |
| Eccentricity: | 0.0004054 |
| inclination: | 36.9657° |
| perigee height: | 528 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 175.9843° |
| argument of perigee: | 44.1485° |
| revolutions per day: | 15.11677889 |
| mean anomaly at epoch: | 315.9584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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