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 59313U 26145.45295218 +.00000000 +00000-0 +44819-3 0 00007
2 59313 42.9995 149.4490 0001679 90.7760 269.3285 15.30528123 09
| Epoch (UTC): | 25 May 2026 10:52:15 |
| Eccentricity: | 0.0001679 |
| inclination: | 42.9995° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 149.4490° |
| argument of perigee: | 90.7760° |
| revolutions per day: | 15.30528123 |
| mean anomaly at epoch: | 269.3285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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