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 67360U 26145.41425485 +.00000000 +00000-0 +51162-3 0 00004
2 67360 43.0055 154.1374 0001832 261.1130 98.9515 15.27590929 00
| Epoch (UTC): | 25 May 2026 09:56:31 |
| Eccentricity: | 0.0001832 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.1374° |
| argument of perigee: | 261.1130° |
| revolutions per day: | 15.27590929 |
| mean anomaly at epoch: | 98.9515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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