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 52838U 26145.45612053 +.00000000 +00000-0 +60981-3 0 00000
2 52838 53.2133 49.4926 0001410 95.7019 264.4134 15.08792574 08
| Epoch (UTC): | 25 May 2026 10:56:48 |
| Eccentricity: | 0.0001410 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.4926° |
| argument of perigee: | 95.7019° |
| revolutions per day: | 15.08792574 |
| mean anomaly at epoch: | 264.4134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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