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 52879U 26145.08994462 +.00000000 +00000-0 +61423-4 0 00004
2 52879 53.2132 31.1451 0001398 78.5280 281.5870 15.08839969 04
| Epoch (UTC): | 25 May 2026 02:09:31 |
| Eccentricity: | 0.0001398 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 31.1451° |
| argument of perigee: | 78.5280° |
| revolutions per day: | 15.08839969 |
| mean anomaly at epoch: | 281.5870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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