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 67637U 26145.12120788 +.00000000 +00000-0 +75360-3 0 00003
2 67637 43.0030 68.0589 0001722 272.3205 87.7449 15.27591911 00
| Epoch (UTC): | 25 May 2026 02:54:32 |
| Eccentricity: | 0.0001722 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 68.0589° |
| argument of perigee: | 272.3205° |
| revolutions per day: | 15.27591911 |
| mean anomaly at epoch: | 87.7449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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