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 68735U 26145.58335647 +.00000000 +00000-0 -41925-1 0 00004
2 68735 97.2845 9.2512 0002054 79.4062 286.2087 15.51645844 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002054 |
| inclination: | 97.2845° |
| perigee height: | 411 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 9.2512° |
| argument of perigee: | 79.4062° |
| revolutions per day: | 15.51645844 |
| mean anomaly at epoch: | 286.2087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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