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 52872U 26145.40738215 +.00000000 +00000-0 +37306-4 0 00008
2 52872 53.2139 29.6936 0001394 85.0404 275.0747 15.08837521 04
| Epoch (UTC): | 25 May 2026 09:46:37 |
| Eccentricity: | 0.0001394 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.6936° |
| argument of perigee: | 85.0404° |
| revolutions per day: | 15.08837521 |
| mean anomaly at epoch: | 275.0747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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