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 67821U 26145.44509029 +.00000000 +00000-0 +62734-3 0 00003
2 67821 43.0041 193.5020 0001656 254.3261 105.7408 15.27592101 07
| Epoch (UTC): | 25 May 2026 10:40:55 |
| Eccentricity: | 0.0001656 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.5020° |
| argument of perigee: | 254.3261° |
| revolutions per day: | 15.27592101 |
| mean anomaly at epoch: | 105.7408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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