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 67627U 26145.05325056 +.00000000 +00000-0 +66545-3 0 00004
2 67627 43.0025 68.4176 0001571 274.4087 85.6585 15.27597250 02
| Epoch (UTC): | 25 May 2026 01:16:40 |
| Eccentricity: | 0.0001571 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 68.4176° |
| argument of perigee: | 274.4087° |
| revolutions per day: | 15.27597250 |
| mean anomaly at epoch: | 85.6585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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