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 52837U 26145.45243156 +.00000000 +00000-0 +64347-4 0 00004
2 52837 53.2132 49.5185 0001777 89.8981 270.2215 15.08834456 03
| Epoch (UTC): | 25 May 2026 10:51:30 |
| Eccentricity: | 0.0001777 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.5185° |
| argument of perigee: | 89.8981° |
| revolutions per day: | 15.08834456 |
| mean anomaly at epoch: | 270.2215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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