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 67064U 26145.18517337 +.00000000 +00000-0 +89436-4 0 00003
2 67064 49.9985 107.8536 0000830 354.1197 5.9665 13.29325524 07
| Epoch (UTC): | 25 May 2026 04:26:38 |
| Eccentricity: | 0.0000830 |
| inclination: | 49.9985° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 107.8536° |
| argument of perigee: | 354.1197° |
| revolutions per day: | 13.29325524 |
| mean anomaly at epoch: | 5.9665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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