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 44622U 26145.61867905 +.00000000 +00000-0 +12196-3 0 00003
2 44622 98.0488 99.0359 0004894 196.3089 163.7968 14.83001363 02
| Epoch (UTC): | 25 May 2026 14:50:53 |
| Eccentricity: | 0.0004894 |
| inclination: | 98.0488° |
| perigee height: | 616 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 99.0359° |
| argument of perigee: | 196.3089° |
| revolutions per day: | 14.83001363 |
| mean anomaly at epoch: | 163.7968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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