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 44910U 26145.52129176 +.00000000 +00000-0 +00000-0 0 00002
2 44910 4.8635 75.3367 0013103 50.0872 350.1142 1.00268571 03
| Epoch (UTC): | 25 May 2026 12:30:39 |
| Eccentricity: | 0.0013103 |
| inclination: | 4.8635° |
| perigee height: | 35732 km |
| apogee height: | 35843 km |
| right ascension of ascending node: | 75.3367° |
| argument of perigee: | 50.0872° |
| revolutions per day: | 1.00268571 |
| mean anomaly at epoch: | 350.1142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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