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 67953U 26145.62520014 +.00000000 +00000-0 +48895-3 0 00008
2 67953 43.0017 116.5330 0001603 266.7086 93.3583 15.27571463 03
| Epoch (UTC): | 25 May 2026 15:00:17 |
| Eccentricity: | 0.0001603 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 116.5330° |
| argument of perigee: | 266.7086° |
| revolutions per day: | 15.27571463 |
| mean anomaly at epoch: | 93.3583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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