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 52989U 26145.66668980 +.00000000 +00000-0 +24956-2 0 00001
2 52989 53.2182 113.5090 0001473 95.5723 72.6090 15.33931082 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001473 |
| inclination: | 53.2182° |
| perigee height: | 463 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 113.5090° |
| argument of perigee: | 95.5723° |
| revolutions per day: | 15.33931082 |
| mean anomaly at epoch: | 72.6090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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