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 59490U 26145.64758567 +.00000000 +00000-0 -93902-4 0 00004
2 59490 42.9992 276.5413 0001063 267.2945 92.7785 15.27569352 00
| Epoch (UTC): | 25 May 2026 15:32:31 |
| Eccentricity: | 0.0001063 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.5413° |
| argument of perigee: | 267.2945° |
| revolutions per day: | 15.27569352 |
| mean anomaly at epoch: | 92.7785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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