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 67597U 26145.45335765 +.00000000 +00000-0 +58124-3 0 00006
2 67597 97.2851 210.6577 0000576 85.4614 274.6694 15.33460454 05
| Epoch (UTC): | 25 May 2026 10:52:50 |
| Eccentricity: | 0.0000576 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.6577° |
| argument of perigee: | 85.4614° |
| revolutions per day: | 15.33460454 |
| mean anomaly at epoch: | 274.6694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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