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 52000U 26145.38939777 +.00000000 +00000-0 +11671-3 0 00000
2 52000 53.2132 34.7125 0001430 92.2282 267.8874 15.08834171 00
| Epoch (UTC): | 25 May 2026 09:20:43 |
| Eccentricity: | 0.0001430 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.7125° |
| argument of perigee: | 92.2282° |
| revolutions per day: | 15.08834171 |
| mean anomaly at epoch: | 267.8874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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