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 52998U 26145.18929896 +.00000000 +00000-0 +13091-4 0 00004
2 52998 53.2140 110.6112 0001329 61.8394 298.2732 15.08839229 08
| Epoch (UTC): | 25 May 2026 04:32:35 |
| Eccentricity: | 0.0001329 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.6112° |
| argument of perigee: | 61.8394° |
| revolutions per day: | 15.08839229 |
| mean anomaly at epoch: | 298.2732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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