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 40697U 26153.94896014 +.00000000 +00000-0 +52850-4 0 00001
2 40697 98.5687 229.0019 0001062 87.4502 272.6803 14.30819267 08
| Epoch (UTC): | 02 June 2026 22:46:30 |
| Eccentricity: | 0.0001062 |
| inclination: | 98.5687° |
| perigee height: | 788 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 229.0019° |
| argument of perigee: | 87.4502° |
| revolutions per day: | 14.30819267 |
| mean anomaly at epoch: | 272.6803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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