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 44637U 26145.52900513 +.00000000 +00000-0 +00000-0 0 00000
2 44637 0.0450 268.3577 0005405 123.1095 125.6123 1.00272730 00
| Epoch (UTC): | 25 May 2026 12:41:46 |
| Eccentricity: | 0.0005405 |
| inclination: | 0.0450° |
| perigee height: | 35764 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 268.3577° |
| argument of perigee: | 123.1095° |
| revolutions per day: | 1.00272730 |
| mean anomaly at epoch: | 125.6123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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