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 52383U 26145.39309078 +.00000000 +00000-0 +37741-4 0 00007
2 52383 53.2113 194.8156 0001023 112.7799 247.3301 15.08842239 06
| Epoch (UTC): | 25 May 2026 09:26:03 |
| Eccentricity: | 0.0001023 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 194.8156° |
| argument of perigee: | 112.7799° |
| revolutions per day: | 15.08842239 |
| mean anomaly at epoch: | 247.3301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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