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 44530U 26145.60657744 +.00000000 +00000-0 +78375-3 0 00009
2 44530 98.6403 309.0406 0008618 31.7317 328.4406 14.71808800 09
| Epoch (UTC): | 25 May 2026 14:33:28 |
| Eccentricity: | 0.0008618 |
| inclination: | 98.6403° |
| perigee height: | 649 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 309.0406° |
| argument of perigee: | 31.7317° |
| revolutions per day: | 14.71808800 |
| mean anomaly at epoch: | 328.4406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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