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 52377U 26145.53939603 +.00000000 +00000-0 -41445-5 0 00007
2 52377 53.2125 204.3501 0001277 88.7512 271.3626 15.08839665 05
| Epoch (UTC): | 25 May 2026 12:56:43 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 204.3501° |
| argument of perigee: | 88.7512° |
| revolutions per day: | 15.08839665 |
| mean anomaly at epoch: | 271.3626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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