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 40303U 26088.20717216 +.00000000 +00000-0 +20124-3 0 00005
2 40303 97.1713 9.4506 0948480 29.5463 335.5970 13.15245809 06
| Epoch (UTC): | 29 March 2026 04:58:19 |
| Eccentricity: | 0.0948480 |
| inclination: | 97.1713° |
| perigee height: | 484 km |
| apogee height: | 1922 km |
| right ascension of ascending node: | 9.4506° |
| argument of perigee: | 29.5463° |
| revolutions per day: | 13.15245809 |
| mean anomaly at epoch: | 335.5970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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