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 44207U 26145.39911447 +.00000000 +00000-0 +81563-4 0 00003
2 44207 97.4800 149.6389 0001579 112.5925 247.5476 15.16749358 08
| Epoch (UTC): | 25 May 2026 09:34:43 |
| Eccentricity: | 0.0001579 |
| inclination: | 97.4800° |
| perigee height: | 515 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 149.6389° |
| argument of perigee: | 112.5925° |
| revolutions per day: | 15.16749358 |
| mean anomaly at epoch: | 247.5476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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