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 52689U 26145.51408147 +.00000000 +00000-0 +10008-2 0 00002
2 52689 53.2075 70.7492 0005120 79.4596 280.6998 15.66975874 01
| Epoch (UTC): | 25 May 2026 12:20:16 |
| Eccentricity: | 0.0005120 |
| inclination: | 53.2075° |
| perigee height: | 364 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 70.7492° |
| argument of perigee: | 79.4596° |
| revolutions per day: | 15.66975874 |
| mean anomaly at epoch: | 280.6998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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