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 59352U 26145.16517632 +.00000000 +00000-0 +63696-4 0 00000
2 59352 43.0019 187.5486 0001216 279.3320 80.7394 15.27576798 06
| Epoch (UTC): | 25 May 2026 03:57:51 |
| Eccentricity: | 0.0001216 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 187.5486° |
| argument of perigee: | 279.3320° |
| revolutions per day: | 15.27576798 |
| mean anomaly at epoch: | 80.7394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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