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 67176U 26145.31403227 +.00000000 +00000-0 +38318-3 0 00006
2 67176 43.0016 237.9954 0001379 258.5754 101.4943 15.27581229 02
| Epoch (UTC): | 25 May 2026 07:32:12 |
| Eccentricity: | 0.0001379 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.9954° |
| argument of perigee: | 258.5754° |
| revolutions per day: | 15.27581229 |
| mean anomaly at epoch: | 101.4943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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