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 68880U 26145.29244458 +.00000000 +00000-0 +65123-3 0 00009
2 68880 51.8760 353.3289 0009671 222.6815 137.3421 15.35971318 05
| Epoch (UTC): | 25 May 2026 07:01:07 |
| Eccentricity: | 0.0009671 |
| inclination: | 51.8760° |
| perigee height: | 451 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 353.3289° |
| argument of perigee: | 222.6815° |
| revolutions per day: | 15.35971318 |
| mean anomaly at epoch: | 137.3421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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