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 44209U 26145.39911571 +.00000000 +00000-0 +81064-4 0 00009
2 44209 97.4800 149.6364 0001969 98.3523 261.7933 15.16749232 08
| Epoch (UTC): | 25 May 2026 09:34:43 |
| Eccentricity: | 0.0001969 |
| inclination: | 97.4800° |
| perigee height: | 514 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 149.6364° |
| argument of perigee: | 98.3523° |
| revolutions per day: | 15.16749232 |
| mean anomaly at epoch: | 261.7933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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