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 59282U 26145.59148198 +.00000000 +00000-0 +65254-4 0 00008
2 59282 50.0083 238.1828 0006292 84.8100 275.3533 14.27954978 00
| Epoch (UTC): | 25 May 2026 14:11:44 |
| Eccentricity: | 0.0006292 |
| inclination: | 50.0083° |
| perigee height: | 794 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 238.1828° |
| argument of perigee: | 84.8100° |
| revolutions per day: | 14.27954978 |
| mean anomaly at epoch: | 275.3533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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