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 67389U 26145.46229701 +.00000000 +00000-0 +24985-3 0 00006
2 67389 97.4583 144.8337 0005074 70.7288 289.4494 15.18269063 00
| Epoch (UTC): | 25 May 2026 11:05:42 |
| Eccentricity: | 0.0005074 |
| inclination: | 97.4583° |
| perigee height: | 508 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 144.8337° |
| argument of perigee: | 70.7288° |
| revolutions per day: | 15.18269063 |
| mean anomaly at epoch: | 289.4494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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