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 59301U 26145.49029419 +.00000000 +00000-0 +10073-4 0 00002
2 59301 43.0014 149.7352 0001336 257.4628 102.6074 15.27580715 01
| Epoch (UTC): | 25 May 2026 11:46:01 |
| Eccentricity: | 0.0001336 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.7352° |
| argument of perigee: | 257.4628° |
| revolutions per day: | 15.27580715 |
| mean anomaly at epoch: | 102.6074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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