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 59044U 26145.48061139 +.00000000 +00000-0 +14547-3 0 00009
2 59044 43.0009 309.7825 0001814 275.0693 84.9952 15.27574129 00
| Epoch (UTC): | 25 May 2026 11:32:04 |
| Eccentricity: | 0.0001814 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.7825° |
| argument of perigee: | 275.0693° |
| revolutions per day: | 15.27574129 |
| mean anomaly at epoch: | 84.9952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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