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 59788U 26145.42283397 +.00000000 +00000-0 -12804-4 0 00006
2 59788 43.0027 135.3053 0001172 279.6540 80.4179 15.27586345 04
| Epoch (UTC): | 25 May 2026 10:08:52 |
| Eccentricity: | 0.0001172 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.3053° |
| argument of perigee: | 279.6540° |
| revolutions per day: | 15.27586345 |
| mean anomaly at epoch: | 80.4179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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