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 44322U 26145.54239970 +.00000000 +00000-0 +10793-5 0 00000
2 44322 97.7594 153.3065 0001453 90.1290 270.0096 14.92588461 07
| Epoch (UTC): | 25 May 2026 13:01:03 |
| Eccentricity: | 0.0001453 |
| inclination: | 97.7594° |
| perigee height: | 589 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 153.3065° |
| argument of perigee: | 90.1290° |
| revolutions per day: | 14.92588461 |
| mean anomaly at epoch: | 270.0096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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