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 44495U 26145.20216418 +.00000000 +00000-0 +78720-3 0 00008
2 44495 44.9964 66.0326 0009284 162.1182 198.0050 15.80670729 09
| Epoch (UTC): | 25 May 2026 04:51:06 |
| Eccentricity: | 0.0009284 |
| inclination: | 44.9964° |
| perigee height: | 322 km |
| apogee height: | 335 km |
| right ascension of ascending node: | 66.0326° |
| argument of perigee: | 162.1182° |
| revolutions per day: | 15.80670729 |
| mean anomaly at epoch: | 198.0050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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