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 44881U 26101.46999733 +.00000000 +00000-0 +33937-4 0 00007
2 44881 97.7559 175.3240 0012485 310.9945 49.0190 14.86412478 00
| Epoch (UTC): | 11 April 2026 11:16:47 |
| Eccentricity: | 0.0012485 |
| inclination: | 97.7559° |
| perigee height: | 600 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 175.3240° |
| argument of perigee: | 310.9945° |
| revolutions per day: | 14.86412478 |
| mean anomaly at epoch: | 49.0190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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