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 44885U 26145.60118937 +.00000000 +00000-0 +46244-3 0 00008
2 44885 97.7914 239.6710 0012679 143.0087 217.2015 15.03593811 08
| Epoch (UTC): | 25 May 2026 14:25:42 |
| Eccentricity: | 0.0012679 |
| inclination: | 97.7914° |
| perigee height: | 547 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 239.6710° |
| argument of perigee: | 143.0087° |
| revolutions per day: | 15.03593811 |
| mean anomaly at epoch: | 217.2015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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