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 68684U 26145.10436110 +.00000000 +00000-0 +10917-3 0 00000
2 68684 97.2870 16.7539 0001607 87.0073 273.1353 15.33440412 08
| Epoch (UTC): | 25 May 2026 02:30:16 |
| Eccentricity: | 0.0001607 |
| inclination: | 97.2870° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.7539° |
| argument of perigee: | 87.0073° |
| revolutions per day: | 15.33440412 |
| mean anomaly at epoch: | 273.1353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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