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 52093U 26145.18152426 +.00000000 +00000-0 -12925-5 0 00004
2 52093 53.2151 105.7458 0001523 80.7452 279.3713 15.08834632 07
| Epoch (UTC): | 25 May 2026 04:21:23 |
| Eccentricity: | 0.0001523 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.7458° |
| argument of perigee: | 80.7452° |
| revolutions per day: | 15.08834632 |
| mean anomaly at epoch: | 279.3713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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