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 68492U 26145.32993045 +.00000000 +00000-0 +45875-3 0 00007
2 68492 97.7549 103.8725 0005045 115.1645 245.0098 14.91414700 04
| Epoch (UTC): | 25 May 2026 07:55:05 |
| Eccentricity: | 0.0005045 |
| inclination: | 97.7549° |
| perigee height: | 590 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.8725° |
| argument of perigee: | 115.1645° |
| revolutions per day: | 14.91414700 |
| mean anomaly at epoch: | 245.0098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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