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 52617U 26145.64976520 +.00000000 +00000-0 +85502-4 0 00005
2 52617 53.2132 283.6345 0001002 90.0225 270.0882 15.08839697 04
| Epoch (UTC): | 25 May 2026 15:35:39 |
| Eccentricity: | 0.0001002 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 283.6345° |
| argument of perigee: | 90.0225° |
| revolutions per day: | 15.08839697 |
| mean anomaly at epoch: | 270.0882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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