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 67352U 26145.42053668 +.00000000 +00000-0 +51698-3 0 00000
2 67352 43.0020 153.3176 0001596 260.4309 99.6363 15.27597071 05
| Epoch (UTC): | 25 May 2026 10:05:34 |
| Eccentricity: | 0.0001596 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.3176° |
| argument of perigee: | 260.4309° |
| revolutions per day: | 15.27597071 |
| mean anomaly at epoch: | 99.6363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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