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 67844U 26145.47978978 +.00000000 +00000-0 +51525-3 0 00000
2 67844 42.9994 193.7659 0001591 268.3384 91.7285 15.27590743 03
| Epoch (UTC): | 25 May 2026 11:30:53 |
| Eccentricity: | 0.0001591 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.7659° |
| argument of perigee: | 268.3384° |
| revolutions per day: | 15.27590743 |
| mean anomaly at epoch: | 91.7285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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