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 59281U 26145.61480000 +.00000000 +00000-0 +86452-4 0 00004
2 59281 50.0088 118.1412 0004476 109.4380 250.7018 14.27964609 03
| Epoch (UTC): | 25 May 2026 14:45:18 |
| Eccentricity: | 0.0004476 |
| inclination: | 50.0088° |
| perigee height: | 795 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 118.1412° |
| argument of perigee: | 109.4380° |
| revolutions per day: | 14.27964609 |
| mean anomaly at epoch: | 250.7018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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