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 67399U 26145.24140778 +.00000000 +00000-0 +19156-3 0 00003
2 67399 97.4567 144.7848 0009192 70.4778 289.7449 15.19281554 08
| Epoch (UTC): | 25 May 2026 05:47:37 |
| Eccentricity: | 0.0009192 |
| inclination: | 97.4567° |
| perigee height: | 502 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 144.7848° |
| argument of perigee: | 70.4778° |
| revolutions per day: | 15.19281554 |
| mean anomaly at epoch: | 289.7449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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