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 59283U 26145.63731785 +.00000000 +00000-0 +81308-4 0 00002
2 59283 50.0087 357.9238 0004647 141.4501 218.6747 14.27987131 01
| Epoch (UTC): | 25 May 2026 15:17:44 |
| Eccentricity: | 0.0004647 |
| inclination: | 50.0087° |
| perigee height: | 795 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 357.9238° |
| argument of perigee: | 141.4501° |
| revolutions per day: | 14.27987131 |
| mean anomaly at epoch: | 218.6747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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