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 52371U 26145.54034485 +.00000000 +00000-0 +82197-4 0 00003
2 52371 53.2121 204.1353 0001012 94.3888 265.7219 15.08830248 07
| Epoch (UTC): | 25 May 2026 12:58:05 |
| Eccentricity: | 0.0001012 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 204.1353° |
| argument of perigee: | 94.3888° |
| revolutions per day: | 15.08830248 |
| mean anomaly at epoch: | 265.7219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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