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 67617U 26145.47641404 +.00000000 +00000-0 +69916-3 0 00002
2 67617 43.0034 66.4419 0000703 252.9586 107.1189 15.27582504 06
| Epoch (UTC): | 25 May 2026 11:26:02 |
| Eccentricity: | 0.0000703 |
| inclination: | 43.0034° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.4419° |
| argument of perigee: | 252.9586° |
| revolutions per day: | 15.27582504 |
| mean anomaly at epoch: | 107.1189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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