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 44520U 26145.58759971 +.00000000 +00000-0 +16701-3 0 00005
2 44520 97.7775 159.0152 0011972 64.5220 295.7239 14.96600709 00
| Epoch (UTC): | 25 May 2026 14:06:08 |
| Eccentricity: | 0.0011972 |
| inclination: | 97.7775° |
| perigee height: | 569 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 159.0152° |
| argument of perigee: | 64.5220° |
| revolutions per day: | 14.96600709 |
| mean anomaly at epoch: | 295.7239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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