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 67367U 26145.45836600 +.00000000 +00000-0 +28045-3 0 00004
2 67367 97.7984 144.3593 0007085 207.3159 152.7686 14.88178768 04
| Epoch (UTC): | 25 May 2026 11:00:02 |
| Eccentricity: | 0.0007085 |
| inclination: | 97.7984° |
| perigee height: | 599 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 144.3593° |
| argument of perigee: | 207.3159° |
| revolutions per day: | 14.88178768 |
| mean anomaly at epoch: | 152.7686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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