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 68692U 26131.85708492 +.00000000 +00000-0 +12811-3 0 00006
2 68692 97.6597 207.4737 0015747 180.0003 180.1228 15.09523009 08
| Epoch (UTC): | 11 May 2026 20:34:12 |
| Eccentricity: | 0.0015747 |
| inclination: | 97.6597° |
| perigee height: | 527 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 207.4737° |
| argument of perigee: | 180.0003° |
| revolutions per day: | 15.09523009 |
| mean anomaly at epoch: | 180.1228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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