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 67995U 26145.24023514 +.00000000 +00000-0 +74827-3 0 00009
2 67995 43.0025 336.3905 0001730 262.5562 97.5093 15.27601817 01
| Epoch (UTC): | 25 May 2026 05:45:56 |
| Eccentricity: | 0.0001730 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 336.3905° |
| argument of perigee: | 262.5562° |
| revolutions per day: | 15.27601817 |
| mean anomaly at epoch: | 97.5093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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