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 68792U 26145.37407771 +.00000000 +00000-0 +31463-3 0 00009
2 68792 97.5032 295.2138 0014667 180.7695 179.3512 15.06608330 00
| Epoch (UTC): | 25 May 2026 08:58:40 |
| Eccentricity: | 0.0014667 |
| inclination: | 97.5032° |
| perigee height: | 536 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 295.2138° |
| argument of perigee: | 180.7695° |
| revolutions per day: | 15.06608330 |
| mean anomaly at epoch: | 179.3512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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