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 52098U 26145.11064669 +.00000000 +00000-0 -74144-4 0 00003
2 52098 53.2139 106.0509 0001578 85.0692 275.0480 15.08845053 06
| Epoch (UTC): | 25 May 2026 02:39:19 |
| Eccentricity: | 0.0001578 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 106.0509° |
| argument of perigee: | 85.0692° |
| revolutions per day: | 15.08845053 |
| mean anomaly at epoch: | 275.0480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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