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 67804U 26145.46924878 +.00000000 +00000-0 +55663-3 0 00002
2 67804 97.2840 333.5031 0002742 95.7625 264.3931 15.33462718 02
| Epoch (UTC): | 25 May 2026 11:15:43 |
| Eccentricity: | 0.0002742 |
| inclination: | 97.2840° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.5031° |
| argument of perigee: | 95.7625° |
| revolutions per day: | 15.33462718 |
| mean anomaly at epoch: | 264.3931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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