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 59088U 26145.52298395 +.00000000 +00000-0 +61710-4 0 00003
2 59088 43.0001 236.6638 0001088 244.6082 115.4657 15.27580620 02
| Epoch (UTC): | 25 May 2026 12:33:05 |
| Eccentricity: | 0.0001088 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.6638° |
| argument of perigee: | 244.6082° |
| revolutions per day: | 15.27580620 |
| mean anomaly at epoch: | 115.4657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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