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 67827U 26145.47721741 +.00000000 +00000-0 +84631-3 0 00009
2 67827 43.0004 193.7533 0001741 267.9335 92.1317 15.27586053 07
| Epoch (UTC): | 25 May 2026 11:27:11 |
| Eccentricity: | 0.0001741 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.7533° |
| argument of perigee: | 267.9335° |
| revolutions per day: | 15.27586053 |
| mean anomaly at epoch: | 92.1317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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