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 68909U 26145.51128345 +.00000000 +00000-0 +87094-3 0 00003
2 68909 97.2867 341.2377 0001730 86.1522 273.9927 15.49234821 03
| Epoch (UTC): | 25 May 2026 12:16:14 |
| Eccentricity: | 0.0001730 |
| inclination: | 97.2867° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 341.2377° |
| argument of perigee: | 86.1522° |
| revolutions per day: | 15.49234821 |
| mean anomaly at epoch: | 273.9927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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